Falcon 9

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Falcon 9

Part of Falcon

Falcon 9
Credit: NASA

American low cost orbital launch vehicle. In September 2006 SpaceX was named as one of two winners of the NASA Commercial Orbital Transportation Services competition. The SpaceX award was $278 million for three flight demonstrations of the Falcon 9 booster carrying the Dragon space capsule. On 23 December 2008 NASA announced that the Falcon 9 / Dragon had been selected for launch of a guaranteed minimum of 20,000 kg of payload to the International Space Station in 2010-2014. The firm contract was worth $1.6 billion, with another $1.5 billion of options.

Status: Active. First Launch: 2010-06-04. Last Launch: 2019-01-11. Number: 46 . Payload: 10,450 kg (23,030 lb). Thrust: 5,560.00 kN (1,249,930 lbf). Gross mass: 333,400 kg (735,000 lb). Height: 55.00 m (180.00 ft). Diameter: 3.60 m (11.80 ft). Span: 3.60 m (11.80 ft). Apogee: 200 km (120 mi).

Reliability of the Falcon 9 was assured by a hold-before-release system – the Falcon was held down and could not be released for flight until all propulsion and vehicle systems were confirmed to be operating normally. An automatic safe shut-down and unloading of propellant occurred if any off nominal conditions are detected. A Kevlar shield protects each engine from debris in the event of its neighbor failing. All Falcon designs had only two stages and only one stage separation event – the minimum practical. All stage separation bolts were all dual initiated, fully space qualified, and had a zero failure track record in prior launch vehicles. Guidance was by triple redundant flight computers and inertial navigation, with a GPS overlay for additional orbit insertion accuracy. The engines, structural materials and design principles, avionics and launch system were all to have been proven on earlier Falcon 1 flights before the first Falcon 9 was ever launched.

The Falcon 9 first and second stage tank walls and domes were made from aluminum 2219, using all friction stir welding. The interstage was made of a carbon fiber honeycomb structure. The separation system consisted of pyrotechnic release bolts and pneumatic separation pushers. Although in-flight failures are very rarely explosive, a Kevlar shield protects each engine from debris in the event of its neighbor failing.

LEO Payload: 10,450 kg (23,030 lb) to a 200 km orbit at 28.00 degrees. Payload: 4,540 kg (10,000 lb) to a GTO, 28 deg. Development Cost $: 378.000 million. Launch Price $: 36.750 million in 2008 dollars in 2008 dollars. Boost Propulsion: Lox/Kerosene. Cruise Thrust: 66.600 kN (14,972 lbf). Cruise Thrust: 6,800 kgf. Cruise engine: Kestrel. Initial Operational Capability: 2009.

More at: Falcon 9.

Family: LCLVs, low cost, orbital launch vehicle. Country: USA. Spacecraft: CUSat, DANDE, DSCOVR, MAC-200, Orbital star, SN-100, FS-1300, Star bus, Celestis, HS 702, Cubesat, Spacebus 4000, Dragon. Launch Sites: Vandenberg SLC4E, Cape Canaveral LC40. Agency: SES, SpaceX.

2010 June 4 - . 18:45 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC40. Launch Pad: SLC40. LV Family: Falcon. Launch Vehicle: Falcon 9.

Dragon/Falcon 9 - . Mass: 4,000 kg (8,800 lb). Nation: USA. Agency: SpaceX. Class: Manned. Type: Manned spacecraft. Spacecraft: Dragon. Duration: 23.00 days. Decay Date: 2010-06-27 . USAF Sat Cat: 36595 . COSPAR: 2010-026A. Apogee: 140 km (80 mi). Perigee: 138 km (85 mi). Inclination: 34.50 deg. Period: 87.30 min. First launch of the commercial Falcon 9 launch vehicle. Structural model of Dragon reusable spacecraft. Remained attached to final stage..

2010 December 8 - . 15:43 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC40. Launch Pad: SLC40. LV Family: Falcon. Launch Vehicle: Falcon 9.

Dragon C1 - . Mass: 6,650 kg (14,660 lb). Nation: USA. Class: Manned. Type: Manned spacecraft. Spacecraft: Dragon. Duration: 0.14 days. Decay Date: 2010-01-12 . USAF Sat Cat: 37244 . COSPAR: 2010-066A. Apogee: 306 km (190 mi). Perigee: 281 km (174 mi). Inclination: 34.50 deg. Period: 90.40 min. First test of the Dragon recoverable spacecraft. Splashed down and successfully recovered in the Pacific Ocean 800 km west of Mexico after a 3 hour 20 minute mission..

QBX2 - . Payload: QbX-2. Mass: 1.00 kg (2.20 lb). Nation: USA. Class: Technology. Type: Technology satellite. Spacecraft: Cubesat. Decay Date: 2011-12-31 . USAF Sat Cat: 37245 . COSPAR: 2010-066B. Apogee: 187 km (116 mi). Perigee: 173 km (107 mi). Inclination: 34.50 deg. Period: 88.10 min. 3U cubesat built by Pumpkin Inc of San Francisco for the National Reconaissance Office's Colony-1 technology development project. Successful..

SMDC One - . Payload: SMDC-One. Mass: 4.00 kg (8.80 lb). Nation: USA. Class: Technology. Type: Technology satellite. Spacecraft: Cubesat. Decay Date: 2011-12-31 . USAF Sat Cat: 37246 . COSPAR: 2010-066C. Apogee: 184 km (114 mi). Perigee: 173 km (107 mi). Inclination: 34.50 deg. Period: 88.10 min. Operational Nanosatellite Experiment for the US Army Space and Missile Defense Center.

Perseus 003 - . Mass: 1.00 kg (2.20 lb). Nation: USA. Class: Technology. Type: Technology satellite. Spacecraft: Cubesat. Decay Date: 2010-01-06 . USAF Sat Cat: 37247 . COSPAR: 2010-066D. Apogee: 190 km (110 mi). Perigee: 179 km (111 mi). Inclination: 34.50 deg. Period: 88.20 min. Los Alamos National Laboratory cubesat, perhaps for ionospheric monitoring..

Perseus 001 - . Mass: 1.00 kg (2.20 lb). Nation: USA. Class: Technology. Type: Technology satellite. Spacecraft: Cubesat. Decay Date: 2010-12-30 . USAF Sat Cat: 37248 . COSPAR: 2010-066E. Apogee: 183 km (113 mi). Perigee: 176 km (109 mi). Inclination: 34.50 deg. Period: 88.10 min. Los Alamos National Laboratory cubesat, perhaps for ionospheric monitoring..

QBX1 - . Payload: QbX-1. Mass: 1.00 kg (2.20 lb). Nation: USA. Class: Technology. Type: Technology satellite. Spacecraft: Cubesat. Decay Date: 2011-12-30 . USAF Sat Cat: 37249 . COSPAR: 2010-066F. Apogee: 197 km (122 mi). Perigee: 185 km (114 mi). Inclination: 34.50 deg. Period: 88.30 min. 3U cubesat satellite built by Pumpkin Inc of San Francisco for the National Reconaissance Office's Colony-1 technology development project. Successful..

Perseus 002 - . Mass: 1.00 kg (2.20 lb). Nation: USA. Class: Technology. Type: Technology satellite. Spacecraft: Cubesat. Decay Date: 2010-12-22 . USAF Sat Cat: 37250 . COSPAR: 2010-066G. Apogee: 193 km (119 mi). Perigee: 183 km (113 mi). Inclination: 34.50 deg. Period: 88.20 min. Los Alamos National Laboratory cubesat, perhaps for ionospheric monitoring..

Perseus 000 - . Mass: 1.00 kg (2.20 lb). Nation: USA. Class: Technology. Type: Technology satellite. Spacecraft: Cubesat. Decay Date: 2010-12-30 . USAF Sat Cat: 37251 . COSPAR: 2010-066H. Apogee: 190 km (110 mi). Perigee: 180 km (110 mi). Inclination: 34.50 deg. Period: 88.20 min. Los Alamos National Laboratory cubesat, perhaps for ionospheric monitoring..

Mayflower - . Payload: Caerus/Mayflower. Mass: 3.00 kg (6.60 lb). Nation: USA. Class: Technology. Type: Technology satellite. Spacecraft: Cubesat. Decay Date: 2010-12-22 . USAF Sat Cat: 37252 . COSPAR: 2010-066J. Apogee: 194 km (120 mi). Perigee: 179 km (111 mi). Inclination: 34.50 deg. Period: 88.20 min.
Experiment for Northrop Grumman NovaWorks and the University of Southern California. 3U cubesat with deployable solar panels composed of a Northrop Grumman's 2-unit Mayflower Next Generation Technology Nanosat and University of Southern California's 1-unit cubesat.

2012 May 22 - . 07:44 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC40. Launch Pad: SLC40. LV Family: Falcon. Launch Vehicle: Falcon 9.

Dragon C2 - . Mass: 6,650 kg (14,660 lb). Nation: USA. Program: ISS. Class: Manned. Type: Manned spacecraft. Spacecraft: Dragon. Duration: 9.00 days. Decay Date: 2012-05-31 . USAF Sat Cat: 38348 . COSPAR: 2012-027A. Apogee: 406 km (252 mi). Perigee: 392 km (243 mi). Inclination: 51.60 deg. Period: 92.50 min. First commercial delivery of cargo to a space station. After rendezvous with the International Space Station, it was captured by the station's SSRMS robot arm on 25 May at 13:56 GMT. Berthed at the nadir CBM port of the Harmony module at 16:02 GMT..

Celestis 11 - . Mass: 7.00 kg (15.40 lb). Nation: USA. Class: Burial. Type: Burial satellite. Spacecraft Bus: Pegasus-3. Spacecraft: Celestis. Decay Date: 2012-06-27 . USAF Sat Cat: 38349 . COSPAR: 2012-027B. Apogee: 298 km (185 mi). Perigee: 253 km (157 mi). Inclination: 51.70 deg. Period: 90.00 min. Released from the Dragon spacecraft. Carried some of the ashes of Star Trek actor James Doohan, among others..

2012 October 8 - . 00:35 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC40. Launch Pad: SLC40. LV Family: Falcon. Launch Vehicle: Falcon 9.

Dragon CRS-1 - . Mass: 9,500 kg (20,900 lb). Nation: USA. Program: ISS. Class: Manned. Type: Manned spacecraft. Spacecraft: Dragon. Duration: 20.00 days. Decay Date: 2012-10-28 . USAF Sat Cat: 38846 . COSPAR: 2012-054A. Apogee: 425 km (264 mi). Perigee: 402 km (249 mi). Inclination: 51.60 deg. Period: 92.80 min.
One first stage engine had an anomaly at max Q (T+1:20) with some debris observed falling away; the engine was shut down but the remaining engines and the second stage compensated to reach the initial orbit. However, extra propellant was used and stage two did not restart as planned. Nevertheless Dragon reached the ISS on 10 October and was captured by the station's SSRMS arm at 10:56 GMT and berthed to the Harmony module at 13:03 GMT. Following unloading of the cargo delivered to the ISS and loading of experimental results and failed equipment for return to earth, the SSRMS unberthed Dragon at 11:19 GMT on 28 October and released it at 13:29 GMT. At 14:22 GMT the Dragon made a burn to lower its orbit and at 18:28 GMT came the 10 minute 40 second long deorbit burn. The Dragon trunk was jettisoned at 18:41 GMT and the capsule reached entry interface at 19:02 GMT. Splashdown in the Pacific Ocean was at around 123 deg W 28 deg N at 19:22

Orbcomm OG2-1 - . Mass: 172 kg (379 lb). Nation: USA. Class: Communications. Type: Communications satellite. Spacecraft: SN-100. Decay Date: 2012-10-10 . USAF Sat Cat: 38847 . COSPAR: 2012-054B. Apogee: 204 km (126 mi). Perigee: 145 km (90 mi). Inclination: 51.60 deg. Period: 88.00 min.
The mission's secondary payload, the first Orbcomm Second Generation communications satellite, was sacrificed in order to allow the Dragon cargo ship to reach the ISS after a rocket engine failure in the booster during ascent to orbit. The OG2 was ejected at 01:37 GMT into a 203 km x 323 km orbit instead of its planned 350 km x 750 km insertion orbit. Orbcomm was not be able to get to the operational 750 km x 750 km orbit. Instead the satellite reentered at 06:19 GMT on 10 October after two days in space, probably over the Pacific west of Vancouver, Canada. An Orbcomm press release stated that they were able to test out the satellite's systems before the reentry.

2013 March 1 - . 15:10 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC40. Launch Pad: SLC40. LV Family: Falcon. Launch Vehicle: Falcon 9.

Dragon CRS-2 - . Mass: 9,500 kg (20,900 lb). Nation: USA. Program: ISS. Class: Manned. Type: Manned logistics spacecraft. Spacecraft: Dragon. Duration: 25.00 days. Decay Date: 2013-03-26 . USAF Sat Cat: 39115 . COSPAR: 2013-010A. Apogee: 409 km (254 mi). Perigee: 380 km (230 mi). Inclination: 51.65 deg. Period: 92.44 min.
Initial issues with thrusters and solar panel deployment were solved, but delayed rendezvous with the ISS by one day. Captured by the ISS SSRMS robot arm at 10:31 GMT on 3 March. Delivered 677 kg of cargo in the pressurized section. Externally, two 119 kg grapple fixtures for the ISS Heat Rejection System were delivered. Undocked and released by the SSRMS at 10:56 GMT on 26 March. Retrofire at 15:42 GMT followed by splashdown in the Pacific at 30.52 deg N / 120.04 deg W at 16:35 GMT.

2013 September 29 - . 16:00 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg SLC4E. LV Family: Falcon. Launch Vehicle: Falcon 9.

Cassiope - . Mass: 500 kg (1,100 lb). Nation: Canada. Class: Communications. Type: Communications satellite. Spacecraft: MAC-200. USAF Sat Cat: 39265 . COSPAR: 2013-055A. Apogee: 1,437 km (892 mi). Perigee: 324 km (201 mi). Inclination: 80.99 deg. Period: 102.57 min.
Canadian Space Agency satellite with two payloads: the CASCADE high bandwith Ka-band communications relay package and the ePOP suite of instruments to study the polar ionosphere. The satellite was built by MacDonald, Dettwiler and Associates (MDA Ltd.) using a Bristol Aerospace spacecraft bus. First launch of the Falcon 9 v1.1 upgrade of the Falcon 9 rocket.

CUSat - . Mass: 23 kg (50 lb). Nation: USA. Class: Technology. Type: Technology satellite. Spacecraft: CUSat. USAF Sat Cat: 39266 . COSPAR: 2013-055B. Apogee: 1,426 km (886 mi). Perigee: 323 km (200 mi). Inclination: 80.99 deg. Period: 102.45 min.
Cornell University satellite; carried a differential GPS navigation system and pulsed plasma thrusters. The defunct-before-launch CUSAT 2/Top satellite remained attached to the Falcon 9 second stage. CUSAT (formerly CUSAT 1/Bottom) was launched attached to CUSAT 2 and separated from it after orbit insertion.

DANDE - . Mass: 38 kg (83 lb). Nation: USA. Class: Science. Type: Science satellite. Spacecraft: DANDE. USAF Sat Cat: 39267 . COSPAR: 2013-055C. Apogee: 1,448 km (899 mi). Perigee: 324 km (201 mi). Inclination: 80.99 deg. Period: 102.69 min.
Drag and Atmospheric Neutral Density Explorer from the University of Colorado. The sphere carried a particle spectrometer to measure the outer atmosphere wind speed and direction, and a drag measurement system. It was attached to an 8 kg Lightband adapter which was jettisoned on October 30 (cataloged as 2013-055AC) and DANDE then began its atmospheric density studies.

POPACS 1 - . Mass: 1.00 kg (2.20 lb). Nation: USA. Class: Science. Type: Science satellite. Spacecraft: Cubesat. USAF Sat Cat: 39268 . COSPAR: 2013-055D. Apogee: 1,419 km (881 mi). Perigee: 323 km (200 mi). Inclination: 81.00 deg. Period: 102.37 min. 3U cubesat which split after deployment into four spacer sections that released three 0.10 m diameter aluminium spheres used as passive atmospheric density calibration probes..

POPACS 2 - . Mass: 2.00 kg (4.40 lb). Nation: USA. Class: Science. Type: Science satellite. Spacecraft: Cubesat. USAF Sat Cat: 39269 . COSPAR: 2013-055E. Apogee: 1,440 km (890 mi). Perigee: 323 km (200 mi). Inclination: 81.00 deg. Period: 102.60 min.

POPACS 3 - . Mass: 2.00 kg (4.40 lb). Nation: USA. Class: Science. Type: Science satellite. Spacecraft: Cubesat. USAF Sat Cat: 39270 . COSPAR: 2013-055F. Apogee: 1,451 km (901 mi). Perigee: 324 km (201 mi). Inclination: 81.00 deg. Period: 102.73 min.

2013 December 3 - . 22:41 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC40. Launch Pad: SLC40. LV Family: Falcon. Launch Vehicle: Falcon 9.

SES-8 - . Payload: GeoStar-2.4 Bus. Mass: 3,170 kg (6,980 lb). Nation: SES. Class: Communications. Type: Communications satellite. Spacecraft: Star bus. USAF Sat Cat: 39460 . COSPAR: 2013-071A. Apogee: 35,801 km (22,245 mi). Perigee: 35,774 km (22,228 mi). Inclination: 0.0200 deg. Period: 1,436.13 min.
Communications satellite for SES World Skies. First geostationary launch for Falcon 9 launch vehicle. After reaching parking orbit the second stage reignited at 2308 GMT and placed SES-8 in a 423 x 79,977 km x 20.47 deg supersynchronous transfer orbit. SES-8 used its engine to move into its final geosynchronous orbit.

2014 January 6 - . 22:06 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC40. Launch Pad: SLC40. LV Family: Falcon. Launch Vehicle: Falcon 9.

Thaicom 6 - . Mass: 3,016 kg (6,649 lb). Nation: Thailand. Class: Communications. Type: Communications satellite. Spacecraft: Orbital star. USAF Sat Cat: 39500 . COSPAR: 2014-002A. Apogee: 35,806 km (22,248 mi). Perigee: 35,767 km (22,224 mi). Inclination: 0.0700 deg. Period: 1,436.09 min.
Thaicom Plc of Bangkok communications satellite with Ku and C-band payloads for coverage of southeast Asia, Africa and the Middle East. The initial burn of the Falcon 9 second stage reached a 197 x 497 km parking orbit, and a second burn sent the Thaicom 6 payload to a 375 x 90,039 km x 22.5 deg supersync transfer orbit. By February 3 the satellite had manuevered to a 35,784 x 35,789 km x 0.1 deg geostationary orbit over 78.4 deg East.

2014 April 18 - . 19:25 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC40. Launch Pad: SLC40. LV Family: Falcon. Launch Vehicle: Falcon 9.

Dragon CRS-3 - . Mass: 9,500 kg (20,900 lb). Nation: USA. Program: ISS. Class: Manned. Type: Manned logistics spacecraft. Spacecraft: Dragon. Duration: 30.00 days. Decay Date: 2014-05-18 . USAF Sat Cat: 39680 . COSPAR: 2014-022A. Apogee: 410 km (250 mi). Perigee: 398 km (247 mi). Inclination: 51.65 deg. Period: 92.65 min.
Placed in an initial 313 x 322 km orbit. The first flight of a Falcon 9 with experimental landing legs on the first stage. Falcon 9 stage 1 reignited during descent after reaching around 120 km, and touched down vertically on the ocean after demonstrating that it could maintain its orientation during the return from space. The Falcon 9 second stage carried five cubesats; after ejecting them, the stage was deorbited over the Indian Ocean and destroyed during reentry. The Dragon trunk carried the OPALS and HDEV experiments for laser communications and Earth imaging respectively. They would be installed on the ISS - JSC's HDEV on the Columbus module EPF, and JPL's OPALS for the ELC-1 platform. Spacesuit EMU 3003 was also aboard Dragon. Following unloading of cargo and reloading with items to be returned to earth, the hatch to Dragon CRS-3 was closed on May 17. Dragon was unberthed by the SSRMS Canadarm-2 at about 12:00 GMT May 18 and released at 13:26 GMT. The deorbit burn at 18:12 to 18:22 GMT was followed by trunk separation at about 18:24 GMT, atmosphere entry at 18:45 GMT and splashdown west of Baja California at 19:05 GMT. It was reported that some water leaked into the Dragon cabin after splashdown, but NASA said the cargo was not damaged.

SporeSat - . Mass: 2.00 kg (4.40 lb). Nation: USA. Class: Biology. Type: Biology satellite. Spacecraft: Cubesat. Decay Date: 2014-06-04 . USAF Sat Cat: 39681 . COSPAR: 2014-022B. Apogee: 153 km (95 mi). Perigee: 151 km (93 mi). Inclination: 51.62 deg. Period: 87.54 min. Cubesat for NASA Ames. Released from Falcon second stage..

TSat - . Mass: 2.00 kg (4.40 lb). Nation: USA. Class: Technology. Type: Technology satellite. Spacecraft: Cubesat. Decay Date: 2014-05-28 . USAF Sat Cat: 39682 . COSPAR: 2014-022C. Apogee: 167 km (103 mi). Perigee: 153 km (95 mi). Inclination: 51.61 deg. Period: 87.68 min. Cubesat for Taylor University. Released from Falcon second stage..

All-Star - . Mass: 4.00 kg (8.80 lb). Nation: USA. Class: Science. Type: Science satellite. Spacecraft: Cubesat. Decay Date: 2014-05-26 . USAF Sat Cat: 39683 . COSPAR: 2014-022D. Apogee: 156 km (96 mi). Perigee: 154 km (95 mi). Inclination: 51.64 deg. Period: 87.59 min. Cubesat for the Colorado Space Grant consortium. Released from Falcon second stage..

PhoneSat-2.5 - . Mass: 2.00 kg (4.40 lb). Nation: USA. Class: Technology. Type: Technology satellite. Spacecraft: Cubesat. Decay Date: 2014-05-15 . USAF Sat Cat: 39684 . COSPAR: 2014-022E. Apogee: 119 km (73 mi). Perigee: 109 km (67 mi). Inclination: 51.54 deg. Period: 86.76 min. Cubesat for NASA Ames. Released from Falcon second stage..

Kicksat - . Mass: 3.00 kg (6.60 lb). Nation: USA. Class: Technology. Type: Technology satellite. Spacecraft: Cubesat. Decay Date: 2014-05-14 . USAF Sat Cat: 39685 . COSPAR: 2014-022F. Apogee: 175 km (108 mi). Perigee: 160 km (90 mi). Inclination: 51.65 deg. Period: 87.83 min.
Cubesat for Cornell University's Space Systems Design Stuido. The satellite had a mass of 2.68 kg, of which 0.52 kg was to have been ejected on May 4 in the form of 104 tiny 5-gram Sprites, circuit boards which acted as independent satellites with small transmitters able to send a simple message to ground stations. A timer problem on Kicksat meant that the deployment of the Sprite subsatellites was reset to May 16. However, Kicksat, and its undeployed Sprites, were destroyed when it reentered on May 14.

2014 July 14 - . 15:15 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC40. Launch Pad: SLC40. LV Family: Falcon. Launch Vehicle: Falcon 9.

Orbcomm FM 109 - . Mass: 172 kg (379 lb). Nation: USA. Agency: SPX. Spacecraft: SN-100. USAF Sat Cat: 40086 . COSPAR: 2014-040A. Apogee: 738 km (458 mi). Perigee: 619 km (384 mi). Inclination: 47.00 deg. Period: 98.32 min.
The second stage of the booster deployed a set of six VHF messaging relay satellites for Orbcomm. The second stage carried two ESPA rings (developed for EELV auxilary payloads) each carrying four slots for the 172 kg satellites; the two extra slots were filled with mass dummies which remained attached. The Falcon 9 first stage made a flyback maneuver and deployed landing legs as part of engineering tests for future recovery; the stage was destroyed as it landed on the ocean.

Orbcomm FM 107 - . Mass: 172 kg (379 lb). Nation: USA. Agency: SPX. Spacecraft: SN-100. USAF Sat Cat: 40087 . COSPAR: 2014-040B. Apogee: 738 km (458 mi). Perigee: 619 km (384 mi). Inclination: 47.01 deg. Period: 98.32 min.

Orbcomm FM 106 - . Mass: 172 kg (379 lb). Nation: USA. Agency: SPX. Spacecraft: SN-100. USAF Sat Cat: 40088 . COSPAR: 2014-040C. Apogee: 739 km (459 mi). Perigee: 619 km (384 mi). Inclination: 47.01 deg. Period: 98.33 min.

Orbcomm FM 111 - . Mass: 172 kg (379 lb). Nation: USA. Agency: SPX. Spacecraft: SN-100. USAF Sat Cat: 40089 . COSPAR: 2014-040D. Apogee: 740 km (450 mi). Perigee: 619 km (384 mi). Inclination: 47.01 deg. Period: 98.35 min.

Orbcomm FM 104 - . Mass: 172 kg (379 lb). Nation: USA. Agency: SPX. Spacecraft: SN-100. USAF Sat Cat: 40090 . COSPAR: 2014-040E. Apogee: 740 km (450 mi). Perigee: 619 km (384 mi). Inclination: 47.01 deg. Period: 98.35 min.

Orbcomm FM 103 - . Mass: 172 kg (379 lb). Nation: USA. Agency: SPX. Spacecraft: SN-100. USAF Sat Cat: 40091 . COSPAR: 2014-040F. Apogee: 741 km (460 mi). Perigee: 620 km (380 mi). Inclination: 47.01 deg. Period: 98.37 min.

2014 August 5 - . 08:00 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC40. Launch Pad: SLC40. LV Family: Falcon. Launch Vehicle: Falcon 9.

Asiasat 8 - . Payload: LS-1300LL. Mass: 4,535 kg (9,997 lb). Nation: China. Agency: SPX. Spacecraft: FS-1300. USAF Sat Cat: 40107 . COSPAR: 2014-046A. Apogee: 35,791 km (22,239 mi). Perigee: 35,784 km (22,235 mi). Inclination: 0.0500 deg. Period: 1,436.14 min.
Used an R-4D bipropellant thruster to reach GEO. The first R-4D burn on August 6 raised the orbit from 180 km x 35,762 km x 24.3 deg to 7,137 x 35,751 km x 10.7 deg. By August 11 the satellite was in a 35,725 x 35,732 km x 0.1 deg orbit drifting east over 104 deg E.

2017 May 1 - . 11:14 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC39A. LV Family: Falcon. Launch Vehicle: Falcon 9.

USA 276 - . Payload: NROL-76. Nation: USA. USAF Sat Cat: 42689 . COSPAR: 2017-022A. See NROL 76 (USA 276). ..

2017 May 15 - . 23:20 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC39A. LV Family: Falcon. Launch Vehicle: Falcon 9.

Inmarsat 5F4 - . Nation: USA. USAF Sat Cat: 42698 . COSPAR: 2017-025A. Apogee: 35,788 km (22,237 mi). Perigee: 35,788 km (22,237 mi). Inclination: 0.0200 deg. Period: 1,436.17 min. See Inmarsat-5 F4 (GX 4). ..

2017 June 3 - . 21:06 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC39A. LV Family: Falcon. Launch Vehicle: Falcon 9.

Dragon CRS-11 - . Payload: Dragon C106. Nation: USA. Program: ISS. Class: Manned. Type: Manned logistics spacecraft. Spacecraft: Dragon. USAF Sat Cat: 42744 . COSPAR: 2017-030A. Apogee: 407 km (252 mi). Perigee: 392 km (243 mi). Inclination: 51.64 deg. Period: 92.54 min. See Dragon CRS-11 (SpX 11, Dragon C106-F2). ..

2017 June 3 - . 21:06 GMT - . Launch Platform: ISS. LV Family: Falcon. Launch Vehicle: Falcon 9.

TOKI - . Payload: BIRD-J; BIRD JJ. Nation: Japan. USAF Sat Cat: 42820 . COSPAR: 1998-067MU. Apogee: 319 km (198 mi). Perigee: 318 km (197 mi). Inclination: 51.63 deg. Period: 90.89 min. See Bird J (Toki) ↑. 1U cubesat by Kyushu Institute of Technology. Mission: Technology demonstration. Status as of 2019: Active..

Ghanasat-1 - . Payload: BIRD-G; BIRD GG. Nation: Ghana. USAF Sat Cat: 42821 . COSPAR: 1998-067MV. Apogee: 325 km (201 mi). Perigee: 324 km (201 mi). Inclination: 51.62 deg. Period: 91.02 min. See Bird G (ANUSAT 1) ↑. 1U cubesat by All Nations University. Mission: Technology demonstration. Status as of 2019: Active..

Mazaalai - . Payload: BIRD-M; BIRD MM. Nation: Mongolia. USAF Sat Cat: 42822 . COSPAR: 1998-067MW. Apogee: 322 km (200 mi). Perigee: 321 km (199 mi). Inclination: 51.63 deg. Period: 90.95 min. See Bird M (Mazaalai, NUMSAT 1) ↑. 1U cubesat by National University of Mongolia. Mission: Technology demonstration. Status as of 2019: Active..

BRAC ONNESHA - . Payload: BIRD-B; BIRD BB. Nation: Bangladesh. USAF Sat Cat: 42823 . COSPAR: 1998-067MX. Apogee: 321 km (199 mi). Perigee: 319 km (198 mi). Inclination: 51.63 deg. Period: 90.92 min. See Bird B (BRAC Onnesha) ↑. 1U cubesat by BRAC University. Mission: Technology demonstration. Status as of 2019: Active..

Nigeria EduSat-1 - . Payload: BIRD-N; BIRD NN. Nation: Nigeria. USAF Sat Cat: 42824 . COSPAR: 1998-067MY. Apogee: 323 km (200 mi). Perigee: 321 km (199 mi). Inclination: 51.63 deg. Period: 90.97 min. See Bird N (Nigeria EduSat 1) ↑. 1U cubesat by Federal University of Technology Akure. Mission: Technology demonstration. Status as of 2019: Active..

2017 June 23 - . 19:09 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC39A. LV Family: Falcon. Launch Vehicle: Falcon 9.

BulgariaSat-1 - . Nation: Bulgaria. USAF Sat Cat: 42801 . COSPAR: 2017-038A. Apogee: 35,796 km (22,242 mi). Perigee: 35,776 km (22,230 mi). Inclination: 0.0100 deg. Period: 1,436.07 min. See BulgariaSat 1. ..

2017 June 25 - . 20:24 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg SLC4E. LV Family: Falcon. Launch Vehicle: Falcon 9.

Iridium Next SV113 - . Nation: USA. USAF Sat Cat: 42803 . COSPAR: 2017-039A. Apogee: 779 km (484 mi). Perigee: 776 km (482 mi). Inclination: 86.40 deg. Period: 100.40 min. See Iridium-NEXT 113. ..

Iridium Next SV123 - . Nation: USA. USAF Sat Cat: 42804 . COSPAR: 2017-039B. Apogee: 779 km (484 mi). Perigee: 776 km (482 mi). Inclination: 86.40 deg. Period: 100.40 min. See Iridium-NEXT 123. ..

Iridium Next SV120 - . Nation: USA. USAF Sat Cat: 42805 . COSPAR: 2017-039C. Apogee: 779 km (484 mi). Perigee: 776 km (482 mi). Inclination: 86.40 deg. Period: 100.40 min. See Iridium-NEXT 120. ..

Iridium Next SV115 - . Nation: USA. USAF Sat Cat: 42806 . COSPAR: 2017-039D. Apogee: 748 km (464 mi). Perigee: 747 km (464 mi). Inclination: 86.45 deg. Period: 99.77 min. See Iridium-NEXT 115. ..

Iridium Next SV118 - . Nation: USA. USAF Sat Cat: 42807 . COSPAR: 2017-039E. Apogee: 779 km (484 mi). Perigee: 776 km (482 mi). Inclination: 86.40 deg. Period: 100.40 min. See Iridium-NEXT 118. ..

Iridium Next SV117 - . Nation: USA. USAF Sat Cat: 42808 . COSPAR: 2017-039F. Apogee: 780 km (480 mi). Perigee: 776 km (482 mi). Inclination: 86.40 deg. Period: 100.40 min. See Iridium-NEXT 117. ..

Iridium Next SV126 - . Nation: USA. USAF Sat Cat: 42809 . COSPAR: 2017-039G. Apogee: 779 km (484 mi). Perigee: 776 km (482 mi). Inclination: 86.40 deg. Period: 100.40 min. See Iridium-NEXT 126. ..

Iridium Next SV124 - . Nation: USA. USAF Sat Cat: 42810 . COSPAR: 2017-039H. Apogee: 749 km (465 mi). Perigee: 744 km (462 mi). Inclination: 86.45 deg. Period: 99.75 min. See Iridium-NEXT 124. ..

Iridium Next SV128 - . Nation: USA. USAF Sat Cat: 42811 . COSPAR: 2017-039J. Apogee: 779 km (484 mi). Perigee: 776 km (482 mi). Inclination: 86.39 deg. Period: 100.40 min. See Iridium-NEXT 128. ..

Iridium Next SV121 - . Nation: USA. USAF Sat Cat: 42812 . COSPAR: 2017-039K. Apogee: 779 km (484 mi). Perigee: 776 km (482 mi). Inclination: 86.40 deg. Period: 100.40 min. See Iridium-NEXT 121. ..

2017 July 5 - . 23:37 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC39A. LV Family: Falcon. Launch Vehicle: Falcon 9.

Intelsat IS-35e - . Nation: USA. USAF Sat Cat: 42818 . COSPAR: 2017-041A. Apogee: 35,792 km (22,240 mi). Perigee: 35,782 km (22,233 mi). Inclination: 0.0200 deg. Period: 1,436.12 min. See Intelsat 35e. ..

2017 August 14 - . 16:30 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC39A. LV Family: Falcon. Launch Vehicle: Falcon 9.

Dragon CRS-12 - . Payload: Dragon C113. Nation: USA. Program: ISS. Class: Manned. Type: Manned logistics spacecraft. Spacecraft: Dragon. USAF Sat Cat: 42904 . COSPAR: 2017-045A. Apogee: 398 km (247 mi). Perigee: 393 km (244 mi). Inclination: 51.64 deg. Period: 92.47 min. See Dragon CRS-12 (SpX 12, Dragon C113). ..

2017 August 14 - . 16:30 GMT - . Launch Platform: ISS. LV Family: Falcon. Launch Vehicle: Falcon 9.

KestrelEye IIM - . Payload: KestrelEye II-M; KESTREL EYE 2M. Nation: USA. USAF Sat Cat: 42982 . COSPAR: 1998-067NE. Apogee: 389 km (241 mi). Perigee: 383 km (237 mi). Inclination: 51.64 deg. Period: 92.27 min. See Kestrel Eye 2M ↑. ..

ASTERIA - . Nation: USA. USAF Sat Cat: 43020 . COSPAR: 1998-067NH. Apogee: 373 km (231 mi). Perigee: 371 km (230 mi). Inclination: 51.64 deg. Period: 91.99 min. See ASTERIA ↑. 6U cubesat by NASA. Mission: Technology demonstrator, space telescope. Status as of 2019: Active..

Dellingr - . Nation: USA. USAF Sat Cat: 43021 . COSPAR: 1998-067NJ. Apogee: 386 km (239 mi). Perigee: 384 km (238 mi). Inclination: 51.64 deg. Period: 92.26 min. See Dellingr (ex RBLE) ↑. ..

OSIRIS-3U - . Nation: USA. USAF Sat Cat: 43027 . COSPAR: 1998-067NL. Apogee: 297 km (184 mi). Perigee: 292 km (181 mi). Inclination: 51.63 deg. Period: 90.40 min.
See OSIRIS-3U ↑. 3U cubesat by Pennsylvania State University SSPL. Mission: In situ measurements of temporal and spatial characteristics of ionospheric space weather. Constellation of three 1U spacecraft launched simultaneously.

2017 August 24 - . 18:50 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg SLC4E. LV Family: Falcon. Launch Vehicle: Falcon 9.

FORMOSAT 5 - . Nation: Taiwan. USAF Sat Cat: 42920 . COSPAR: 2017-049A. Apogee: 731 km (454 mi). Perigee: 715 km (444 mi). Inclination: 98.34 deg. Period: 99.25 min. See FORMOSAT 5. ..

2017 September 7 - . 14:00 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC39A. LV Family: Falcon. Launch Vehicle: Falcon 9.

X-37B OTV-5 - . Payload: X-37B No. 2?; OTV 5 (USA 277). Nation: USA. USAF Sat Cat: 42932 . COSPAR: 2017-052A. See X-37B OTV-5 (USA 277). ..

2017 October 9 - . 12:36 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg SLC4E. LV Family: Falcon. Launch Vehicle: Falcon 9.

Iridium Next SV133 - . Nation: USA. USAF Sat Cat: 42955 . COSPAR: 2017-061A. Apogee: 779 km (484 mi). Perigee: 776 km (482 mi). Inclination: 86.39 deg. Period: 100.40 min. See Iridium-NEXT 100 (ex Iridium-NEXT 127). ..

Iridium Next SV127 - . Payload: Iridium Next SV127 (SV100; IRIDIUM 100. Nation: USA. USAF Sat Cat: 42956 . COSPAR: 2017-061B. Apogee: 779 km (484 mi). Perigee: 776 km (482 mi). Inclination: 86.39 deg. Period: 100.40 min. See Iridium-NEXT 107. ..

Iridium Next SV122 - . Nation: USA. USAF Sat Cat: 42957 . COSPAR: 2017-061C. Apogee: 779 km (484 mi). Perigee: 776 km (482 mi). Inclination: 86.39 deg. Period: 100.40 min. See Iridium-NEXT 122. ..

Iridium Next SV129 - . Nation: USA. USAF Sat Cat: 42958 . COSPAR: 2017-061D. Apogee: 779 km (484 mi). Perigee: 776 km (482 mi). Inclination: 86.39 deg. Period: 100.40 min. See Iridium-NEXT 129. ..

Iridium Next SV119 - . Nation: USA. USAF Sat Cat: 42959 . COSPAR: 2017-061E. Apogee: 779 km (484 mi). Perigee: 776 km (482 mi). Inclination: 86.39 deg. Period: 100.40 min. See Iridium-NEXT 119. ..

Iridium Next SV107 - . Nation: USA. USAF Sat Cat: 42960 . COSPAR: 2017-061F. Apogee: 779 km (484 mi). Perigee: 776 km (482 mi). Inclination: 86.39 deg. Period: 100.40 min. See Iridium-NEXT 107. ..

Iridium Next SV132 - . Nation: USA. USAF Sat Cat: 42961 . COSPAR: 2017-061G. Apogee: 780 km (480 mi). Perigee: 776 km (482 mi). Inclination: 86.39 deg. Period: 100.40 min. See Iridium-NEXT 132. ..

Iridium Next SV136 - . Nation: USA. USAF Sat Cat: 42962 . COSPAR: 2017-061H. Apogee: 779 km (484 mi). Perigee: 776 km (482 mi). Inclination: 86.39 deg. Period: 100.40 min. See Iridium-NEXT 136. ..

Iridium Next SV139 - . Nation: USA. USAF Sat Cat: 42963 . COSPAR: 2017-061J. Apogee: 779 km (484 mi). Perigee: 776 km (482 mi). Inclination: 86.39 deg. Period: 100.40 min. See Iridium-NEXT 139. ..

Iridium Next SV125 - . Nation: USA. USAF Sat Cat: 42964 . COSPAR: 2017-061K. Apogee: 779 km (484 mi). Perigee: 776 km (482 mi). Inclination: 86.39 deg. Period: 100.40 min. See Iridium-NEXT 125. ..

2017 October 11 - . 22:52 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC39A. LV Family: Falcon. Launch Vehicle: Falcon 9.

SES-11 - . Nation: SES. USAF Sat Cat: 42967 . COSPAR: 2017-063A. Apogee: 35,797 km (22,243 mi). Perigee: 35,777 km (22,230 mi). Inclination: 0.0200 deg. Period: 1,436.12 min. See EchoStar 105/SES 11. ..

2017 October 30 - . 19:33 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC39A. LV Family: Falcon. Launch Vehicle: Falcon 9.

Mugunghwa 5A - . Payload: Koreasat 5A. Nation: Korea South. USAF Sat Cat: 42984 . COSPAR: 2017-067A. Apogee: 35,792 km (22,240 mi). Perigee: 35,783 km (22,234 mi). Inclination: 0.0100 deg. Period: 1,436.15 min. See Koreasat 5A (Mugungwha 5A). ..

2017 December 15 - . 15:35 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC40. LV Family: Falcon. Launch Vehicle: Falcon 9.

Dragon CRS-13 - . Payload: Dragon C108. Nation: USA. Program: ISS. Class: Manned. Type: Manned logistics spacecraft. Spacecraft: Dragon. USAF Sat Cat: 43060 . COSPAR: 2017-080A. Apogee: 407 km (252 mi). Perigee: 393 km (244 mi). Inclination: 51.65 deg. Period: 92.56 min. See Dragon CRS-13 (SpX 13, Dragon C108-F2). ..

2017 December 23 - . 01:26 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg SLC4E. LV Family: Falcon. Launch Vehicle: Falcon 9.

Iridium Next SV135 - . Nation: USA. USAF Sat Cat: 43070 . COSPAR: 2017-083A. Apogee: 779 km (484 mi). Perigee: 776 km (482 mi). Inclination: 86.40 deg. Period: 100.40 min. See Iridium-NEXT 116. ..

Iridium Next SV138 - . Nation: USA. USAF Sat Cat: 43071 . COSPAR: 2017-083B. Apogee: 779 km (484 mi). Perigee: 776 km (482 mi). Inclination: 86.40 deg. Period: 100.40 min. See Iridium-NEXT 138. ..

Iridium Next SV116 - . Nation: USA. USAF Sat Cat: 43072 . COSPAR: 2017-083C. Apogee: 779 km (484 mi). Perigee: 776 km (482 mi). Inclination: 86.40 deg. Period: 100.40 min. See Iridium-NEXT 116. ..

Iridium Next SV130 - . Nation: USA. USAF Sat Cat: 43073 . COSPAR: 2017-083D. Apogee: 779 km (484 mi). Perigee: 776 km (482 mi). Inclination: 86.40 deg. Period: 100.40 min. See Iridium-NEXT 130. ..

Iridium Next SV151 - . Nation: USA. USAF Sat Cat: 43074 . COSPAR: 2017-083E. Apogee: 779 km (484 mi). Perigee: 776 km (482 mi). Inclination: 86.40 deg. Period: 100.40 min. See Iridium-NEXT 151. ..

Iridium Next SV134 - . Nation: USA. USAF Sat Cat: 43075 . COSPAR: 2017-083F. Apogee: 780 km (480 mi). Perigee: 776 km (482 mi). Inclination: 86.40 deg. Period: 100.40 min. See Iridium-NEXT 134. ..

Iridium Next SV137 - . Nation: USA. USAF Sat Cat: 43076 . COSPAR: 2017-083G. Apogee: 779 km (484 mi). Perigee: 776 km (482 mi). Inclination: 86.40 deg. Period: 100.40 min. See Iridium-NEXT 137. ..

Iridium Next SV141 - . Nation: USA. USAF Sat Cat: 43077 . COSPAR: 2017-083H. Apogee: 779 km (484 mi). Perigee: 776 km (482 mi). Inclination: 86.40 deg. Period: 100.40 min. See Iridium-NEXT 141. ..

Iridium Next SV153 - . Nation: USA. USAF Sat Cat: 43078 . COSPAR: 2017-083J. Apogee: 779 km (484 mi). Perigee: 776 km (482 mi). Inclination: 86.40 deg. Period: 100.40 min. See Iridium-NEXT 153. ..

Iridium Next SV131 - . Nation: USA. USAF Sat Cat: 43079 . COSPAR: 2017-083K. Apogee: 779 km (484 mi). Perigee: 776 km (482 mi). Inclination: 86.40 deg. Period: 100.40 min. See Iridium-NEXT 131. ..

2018 January 8 - . 01:00 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC40. LV Family: Falcon. Launch Vehicle: Falcon 9.

USA 280 - . Payload: ZUMA. Nation: USA. USAF Sat Cat: 43098 . COSPAR: 2018-001A. See Zuma (USA 280). ..

2018 January 31 - . 21:24 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC40. LV Family: Falcon. Launch Vehicle: Falcon 9.

GovSat-1 - . Payload: SES-16; SES-16/GOVSAT-1. Nation: SES. USAF Sat Cat: 43178 . COSPAR: 2018-013A. See GovSat 1 (SES 16). ..

2018 February 22 - . 14:16 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg SLC4E. LV Family: Falcon. Launch Vehicle: Falcon 9.

Paz - . Nation: Spain. USAF Sat Cat: 43215 . COSPAR: 2018-020A. Apogee: 510 km (310 mi). Perigee: 507 km (315 mi). Inclination: 97.45 deg. Period: 94.79 min. See Paz. ..

Tintin A - . Payload: Starlink Demo 1. Nation: USA. USAF Sat Cat: 43216 . COSPAR: 2018-020B. Apogee: 516 km (320 mi). Perigee: 497 km (308 mi). Inclination: 97.45 deg. Period: 94.75 min. See MicroSat 2a (Tintin A). ..

Tintin B - . Payload: Starlink Demo 2. Nation: USA. USAF Sat Cat: 43217 . COSPAR: 2018-020C. Apogee: 515 km (320 mi). Perigee: 497 km (308 mi). Inclination: 97.46 deg. Period: 94.75 min. See MicroSat 2b (Tintin B). ..

2018 March 6 - . 05:32 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC40. LV Family: Falcon. Launch Vehicle: Falcon 9.

Hispasat 30W-6 - . Nation: Spain. USAF Sat Cat: 43228 . COSPAR: 2018-023A. Apogee: 35,805 km (22,248 mi). Perigee: 35,766 km (22,223 mi). Inclination: 0.0400 deg. Period: 1,436.04 min. See Hispasat 30W-6. ..

PODSAT - . Nation: USA. USAF Sat Cat: 43229 . COSPAR: 2018-023B. Apogee: 20,726 km (12,878 mi). Perigee: 172 km (106 mi). Inclination: 26.87 deg. Period: 362.06 min. See PODSAT 1. ..

2018 March 30 - . 14:12 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg SLC4E. LV Family: Falcon. Launch Vehicle: Falcon 9.

Iridium Next SV144 - . Nation: USA. USAF Sat Cat: 43249 . COSPAR: 2018-030A. Apogee: 781 km (485 mi). Perigee: 775 km (481 mi). Inclination: 86.39 deg. Period: 100.40 min. See Iridium-NEXT 140. ..

Iridium Next SV149 - . Nation: USA. USAF Sat Cat: 43250 . COSPAR: 2018-030B. Apogee: 780 km (480 mi). Perigee: 776 km (482 mi). Inclination: 86.40 deg. Period: 100.40 min. See Iridium-NEXT 149. ..

Iridium Next SV157 - . Nation: USA. USAF Sat Cat: 43251 . COSPAR: 2018-030C. Apogee: 779 km (484 mi). Perigee: 777 km (482 mi). Inclination: 86.40 deg. Period: 100.40 min. See Iridium-NEXT 157. ..

Iridium Next SV140 - . Nation: USA. USAF Sat Cat: 43252 . COSPAR: 2018-030D. Apogee: 780 km (480 mi). Perigee: 775 km (481 mi). Inclination: 86.40 deg. Period: 100.40 min. See Iridium-NEXT 140. ..

Iridium Next SV145 - . Nation: USA. USAF Sat Cat: 43253 . COSPAR: 2018-030E. Apogee: 780 km (480 mi). Perigee: 775 km (481 mi). Inclination: 86.40 deg. Period: 100.40 min. See Iridium-NEXT 145. ..

Iridium Next SV146 - . Nation: USA. USAF Sat Cat: 43254 . COSPAR: 2018-030F. Apogee: 779 km (484 mi). Perigee: 776 km (482 mi). Inclination: 86.40 deg. Period: 100.40 min. See Iridium-NEXT 146. ..

Iridium Next SV148 - . Nation: USA. USAF Sat Cat: 43255 . COSPAR: 2018-030G. Apogee: 779 km (484 mi). Perigee: 776 km (482 mi). Inclination: 86.40 deg. Period: 100.40 min. See Iridium-NEXT 148. ..

Iridium Next SV142 - . Nation: USA. USAF Sat Cat: 43256 . COSPAR: 2018-030H. Apogee: 779 km (484 mi). Perigee: 776 km (482 mi). Inclination: 86.40 deg. Period: 100.40 min. See Iridium-NEXT 142. ..

Iridium Next SV150 - . Nation: USA. USAF Sat Cat: 43257 . COSPAR: 2018-030J. Apogee: 779 km (484 mi). Perigee: 776 km (482 mi). Inclination: 86.40 deg. Period: 100.40 min. See Iridium-NEXT 150. ..

Iridium Next SV143 - . Nation: USA. USAF Sat Cat: 43258 . COSPAR: 2018-030K. Apogee: 780 km (480 mi). Perigee: 776 km (482 mi). Inclination: 86.40 deg. Period: 100.40 min. See Iridium-NEXT 143. ..

2018 April 2 - . 20:29 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC40. LV Family: Falcon. Launch Vehicle: Falcon 9.

Dragon CRS-14 - . Payload: Dragon C110. Nation: USA. Program: ISS. Class: Manned. Type: Manned logistics spacecraft. Spacecraft: Dragon. USAF Sat Cat: 43267 . COSPAR: 2018-032A. Apogee: 407 km (252 mi). Perigee: 402 km (249 mi). Inclination: 51.64 deg. Period: 92.65 min. See Dragon CRS-14 (SpX 14). ..

DebrisSat-1 - . COSPAR: 2018-032. See DebrisSat 1 ↑. ..

DebrisSat-2 - . COSPAR: 2018-032. See DebrisSat 2 ↑. ..

2018 April 2 - . 20:29 GMT - . Launch Platform: ISS. LV Family: Falcon. Launch Vehicle: Falcon 9.

UBAKUSAT - . Payload: UBAK-3U-SAT. Nation: Turkey. USAF Sat Cat: 43466 . COSPAR: 1998-067NP. Apogee: 384 km (238 mi). Perigee: 383 km (237 mi). Inclination: 51.64 deg. Period: 92.22 min.
See UBAKUSAT (UBAK-3U-SAT) ↑. 1U cubesat by Istanbul Technical University. Mission: Technology demonstration and Earth observation satellite to provide voice communications for amateur radio stations. Status as of 2019: Active. .

1KUNS-PF - . Nation: Kenya. USAF Sat Cat: 43467 . COSPAR: 1998-067NQ. Apogee: 390 km (240 mi). Perigee: 387 km (240 mi). Inclination: 51.64 deg. Period: 92.32 min.
See 1KUNS-PF ↑. 1U cubesat by University of Nairobi. Mission: Mapping of Kenya's land mass, monitoring of the coastline and helping combat illegal logging activities. Status as of 2019: Active. .

Batsu-CS1 - . Payload: Irazu. Nation: Costa Rica. USAF Sat Cat: 43468 . COSPAR: 1998-067NR. Apogee: 380 km (230 mi). Perigee: 379 km (235 mi). Inclination: 51.64 deg. Period: 92.15 min. See Irazú (Batsú-CS 1) ↑. 1U cubesat by Costa Rica Institute of Technology. Mission: Monitoring carbon, humidity, and temperature levels in Costa Rican forests. Status as of 2019: Active..

RemoveDebris - . Nation: UK. USAF Sat Cat: 43510 . COSPAR: 1998-067NT. Apogee: 401 km (249 mi). Perigee: 396 km (246 mi). Inclination: 51.64 deg. Period: 92.53 min. See RemoveDEBRIS (RemDeb) ↑. ..

2018 April 18 - . 22:50 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC40. LV Family: Falcon. Launch Vehicle: Falcon 9.

TESS - . Nation: USA. USAF Sat Cat: 43435 . COSPAR: 2018-038A. Apogee: 355,637 km (220,982 mi). Perigee: 1,056 km (656 mi). Inclination: 28.91 deg. Period: 13,168.80 min. See TESS (MIDEX 7, Explorer 95). ..

2018 May 11 - . 20:13 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC39A. LV Family: Falcon. Launch Vehicle: Falcon 9.

Bangabandhu 1 - . Nation: Bangladesh. USAF Sat Cat: 43463 . COSPAR: 2018-044A. Apogee: 35,793 km (22,240 mi). Perigee: 35,782 km (22,233 mi). Inclination: 0.0100 deg. Period: 1,436.12 min. See Bangabandhu 1 (BD 1). ..

2018 May 22 - . 19:46 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg SLC4E. LV Family: Falcon. Launch Vehicle: Falcon 9.

GRACE-FO 1 - . Nation: USA. USAF Sat Cat: 43476 . COSPAR: 2018-047A. Apogee: 507 km (315 mi). Perigee: 482 km (299 mi). Inclination: 89.00 deg. Period: 94.50 min. See GRACE-FO 1. ..

GRACE-FO 2 - . Nation: USA. USAF Sat Cat: 43477 . COSPAR: 2018-047B. Apogee: 507 km (315 mi). Perigee: 482 km (299 mi). Inclination: 89.00 deg. Period: 94.50 min. See GRACE-FO 2. ..

Iridium Next SV161 - . Nation: USA. USAF Sat Cat: 43478 . COSPAR: 2018-047C. Apogee: 749 km (465 mi). Perigee: 746 km (463 mi). Inclination: 86.45 deg. Period: 99.77 min. See Iridium-NEXT 161. ..

Iridium Next SV152 - . Nation: USA. USAF Sat Cat: 43479 . COSPAR: 2018-047D. Apogee: 779 km (484 mi). Perigee: 776 km (482 mi). Inclination: 86.40 deg. Period: 100.40 min. See Iridium-NEXT 152. ..

Iridium Next SV147 - . Nation: USA. USAF Sat Cat: 43480 . COSPAR: 2018-047E. Apogee: 779 km (484 mi). Perigee: 776 km (482 mi). Inclination: 86.40 deg. Period: 100.40 min. See Iridium-NEXT 147. ..

Iridium Next SV110 - . Nation: USA. USAF Sat Cat: 43481 . COSPAR: 2018-047F. Apogee: 780 km (480 mi). Perigee: 776 km (482 mi). Inclination: 86.40 deg. Period: 100.40 min. See Iridium-NEXT 110. ..

Iridium Next SV162 - . Nation: USA. USAF Sat Cat: 43482 . COSPAR: 2018-047G. Apogee: 749 km (465 mi). Perigee: 746 km (463 mi). Inclination: 86.45 deg. Period: 99.77 min. See Iridium-NEXT 162. ..

2018 June 4 - . 04:44 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC40. LV Family: Falcon. Launch Vehicle: Falcon 9.

SES-12 - . Nation: SES. USAF Sat Cat: 43488 . COSPAR: 2018-049A. Apogee: 35,864 km (22,284 mi). Perigee: 35,842 km (22,271 mi). Inclination: 0.0600 deg. Period: 1,439.47 min. See SES 12. ..

2018 June 29 - . 09:41 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC40. LV Family: Falcon. Launch Vehicle: Falcon 9.

Dragon CRS-15 - . Payload: Dragon C111. Nation: USA. Program: ISS. Class: Manned. Type: Manned logistics spacecraft. Spacecraft: Dragon. USAF Sat Cat: 43522 . COSPAR: 2018-055A. Apogee: 409 km (254 mi). Perigee: 402 km (249 mi). Inclination: 51.64 deg. Period: 92.68 min. See Dragon CRS-15 (SpX 15, Dragon C111-F2). ..

Biarri-Squad 3 - . COSPAR: 2018-055. See Biarri-Squad 3 ↑. ..

Biarri-Squad 1 - . COSPAR: 2018-055. See Biarri-Squad 1 ↑. ..

Biarri-Squad 2 - . COSPAR: 2018-055. See Biarri-Squad 2 ↑. ..

Bhutan-1 - . Nation: Japan. COSPAR: 2018-055. See Bird BTN (Bhutan 1) ↑. 1U cubesat by Kyushu Institute of Technology. Mission: Technology demonstration. Status as of 2019: Active..

Maya-1 - . Nation: Japan. COSPAR: 2018-055. See Bird PHL (MAYA 1) ↑. 1U cubesat by Kyushu Institute of Technology. Mission: Technology demonstration. Status as of 2019: Active. ..

UiTMSAT-1 - . Payload: Univ. Tek. MARA-Sat-1. Nation: Malaysia. COSPAR: 2018-055. See Bird MYS (UiTMSAT 1) ↑. 1U cubesat by Universiti Teknologi MARA. Mission: Technology demonstration. Status as of 2019: Active. ..

2018 July 22 - . 05:49 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC40. LV Family: Falcon. Launch Vehicle: Falcon 9.

Telstar 19 Vantage - . Payload: Telstar 19V. Nation: Canada. USAF Sat Cat: 43562 . COSPAR: 2018-059A. Apogee: 35,791 km (22,239 mi). Perigee: 35,778 km (22,231 mi). Inclination: 0.0100 deg. Period: 1,436.00 min. See Telstar 19V. ..

2018 July 25 - . 11:38 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg SLC4E. LV Family: Falcon. Launch Vehicle: Falcon 9.

Iridium Next SV160 - . Nation: USA. USAF Sat Cat: 43569 . COSPAR: 2018-061A. Apogee: 779 km (484 mi). Perigee: 776 km (482 mi). Inclination: 86.40 deg. Period: 100.40 min. See Iridium-NEXT 154 . ..

Iridium Next SV166 - . Nation: USA. USAF Sat Cat: 43570 . COSPAR: 2018-061B. Apogee: 779 km (484 mi). Perigee: 776 km (482 mi). Inclination: 86.40 deg. Period: 100.40 min. See Iridium-NEXT 166. ..

Iridium Next SV158 - . Nation: USA. USAF Sat Cat: 43571 . COSPAR: 2018-061C. Apogee: 779 km (484 mi). Perigee: 776 km (482 mi). Inclination: 86.40 deg. Period: 100.40 min. See Iridium-NEXT 158. ..

Iridium Next SV165 - . Nation: USA. USAF Sat Cat: 43572 . COSPAR: 2018-061D. Apogee: 779 km (484 mi). Perigee: 776 km (482 mi). Inclination: 86.40 deg. Period: 100.40 min. See Iridium-NEXT 165. ..

Iridium Next SV155 - . Nation: USA. USAF Sat Cat: 43573 . COSPAR: 2018-061E. Apogee: 780 km (480 mi). Perigee: 776 km (482 mi). Inclination: 86.40 deg. Period: 100.40 min. See Iridium-NEXT 155. ..

Iridium Next SV154 - . Nation: USA. USAF Sat Cat: 43574 . COSPAR: 2018-061F. Apogee: 779 km (484 mi). Perigee: 776 km (482 mi). Inclination: 86.40 deg. Period: 100.40 min. See Iridium-NEXT 154 . ..

Iridium Next SV163 - . Nation: USA. USAF Sat Cat: 43575 . COSPAR: 2018-061G. Apogee: 779 km (484 mi). Perigee: 776 km (482 mi). Inclination: 86.40 deg. Period: 100.40 min. See Iridium-NEXT 163. ..

Iridium Next SV156 - . Nation: USA. USAF Sat Cat: 43576 . COSPAR: 2018-061H. Apogee: 780 km (480 mi). Perigee: 776 km (482 mi). Inclination: 86.40 deg. Period: 100.40 min. See Iridium-NEXT 156. ..

Iridium Next SV164 - . Nation: USA. USAF Sat Cat: 43577 . COSPAR: 2018-061J. Apogee: 779 km (484 mi). Perigee: 776 km (482 mi). Inclination: 86.40 deg. Period: 100.40 min. See Iridium-NEXT 164. ..

Iridium Next SV159 - . Nation: USA. USAF Sat Cat: 43578 . COSPAR: 2018-061K. Apogee: 779 km (484 mi). Perigee: 776 km (482 mi). Inclination: 86.40 deg. Period: 100.40 min. See Iridium-NEXT 159. ..

2018 August 7 - . 05:17 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC40. LV Family: Falcon. Launch Vehicle: Falcon 9.

Merah Putih - . Payload: Telkom 4; TELKOM-4. Nation: Indonesia. USAF Sat Cat: 43587 . COSPAR: 2018-064A. Apogee: 35,795 km (22,241 mi). Perigee: 35,779 km (22,231 mi). Inclination: 0.0100 deg. Period: 1,436.12 min. See Telkom 4 (Merah Putih). ..

2018 September 10 - . 04:44 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC40. LV Family: Falcon. Launch Vehicle: Falcon 9.

Telstar 18 Vantage - . Payload: Telstar 18V. Nation: Canada. USAF Sat Cat: 43611 . COSPAR: 2018-069A. Apogee: 35,800 km (22,200 mi). Perigee: 35,773 km (22,228 mi). Inclination: 0.0200 deg. Period: 1,436.11 min. See Telstar 18V / APStar 5C. ..

2018 October 8 - . 02:20 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg SLC4E. LV Family: Falcon. Launch Vehicle: Falcon 9.

SAOCOM 1A - . Nation: Argentina. USAF Sat Cat: 43641 . COSPAR: 2018-076A. Apogee: 624 km (387 mi). Perigee: 622 km (386 mi). Inclination: 97.89 deg. Period: 97.16 min. See SAOCOM 1A. ..

2018 November 15 - . 20:45 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC39A. LV Family: Falcon. Launch Vehicle: Falcon 9.

Es'hailsat-2 - . Nation: TBD. Type: Comms. USAF Sat Cat: 43700 . COSPAR: 2018-090A. Apogee: 35,791 km (22,239 mi). Perigee: 35,784 km (22,235 mi). Inclination: 0.0200 deg. Period: 1,436.13 min. See Es'hail 2/AMSAT P4A. ..

2018 December 3 - . 18:33 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg SLC4E. LV Family: Falcon. Launch Vehicle: Falcon 9.

MinXSS 2 - . Nation: USA. Type: Solar X. Spacecraft: Cubesat. USAF Sat Cat: 43758 . COSPAR: 2018-099A. Apogee: 593 km (368 mi). Perigee: 570 km (350 mi). Inclination: 97.76 deg. Period: 96.30 min. See MinXSS 2. Astronomy cubesat for U Colorado Boulder; Solar x-ray data. 1017LT SSO..

SSO-A UFF - . Nation: USA. Type: Tech. USAF Sat Cat: 43760 . COSPAR: 2018-099C. Apogee: 593 km (368 mi). Perigee: 572 km (355 mi). Inclination: 97.76 deg. Period: 96.32 min. 1017LT SSO.

Elysium Star 2 - . Nation: USA. Type: Burial. Spacecraft: Cubesat. COSPAR: 2018-099C. See Elysium-Star 2. Burial 1U cubesat for Elysium Space, San Francisco. 1017LT SSO..

ICEYE-X2 - . Nation: TBD. Type: Radar. USAF Sat Cat: 43761 . COSPAR: 2018-099D. Apogee: 593 km (368 mi). Perigee: 572 km (355 mi). Inclination: 97.76 deg. Period: 96.32 min. See ICEYE X2. 1017LT SSO..

STPSat 5 - . Nation: USA. Type: Tech. USAF Sat Cat: 43762 . COSPAR: 2018-099E. Apogee: 591 km (367 mi). Perigee: 571 km (354 mi). Inclination: 97.76 deg. Period: 96.29 min. See STPSat 5. 1017LT SSO..

SSO-A LFF - . Nation: USA. Type: Tech. USAF Sat Cat: 43763 . COSPAR: 2018-099F. Apogee: 591 km (367 mi). Perigee: 571 km (354 mi). Inclination: 97.76 deg. Period: 96.29 min. 1017LT SSO.

Blackhawk - . Type: Comms. Spacecraft: Cubesat. COSPAR: 2018-099. See BlackHawk. Communications technology cubesat for Viasat/Blue Canyon. 1017LT SSO..

Orbital Reflector - . Nation: USA. Type: Art. Spacecraft: Cubesat. COSPAR: 2018-099. See Orbital Reflector (ORS 1). Art cubesat for Nevada Museum of Art, Trevor Paglen. 1017LT SSO..

ICE-Cap - . Type: Comms. Spacecraft: Cubesat. COSPAR: 2018-099. See ICE-Cap. 1017LT SSO..

KNACKSAT - . Nation: Thailand. Type: Tech. Spacecraft: Cubesat. COSPAR: 2018-099. See KNACKSAT. Amateur radio cubesat for King Mongkut Univ of Tech., Bangkok. 1017LT SSO..

RAAF M1 - . Nation: Australia. Type: Comms. Spacecraft: Cubesat. COSPAR: 2018-099. See RAAF M1. AIS/ADS-B maritime/aviavtion location cubesat for Royal Australian AF, UNSW. 1017LT SSO..

DoD Cube 2C - . Nation: USA. Type: Comms?. Spacecraft: Cubesat. COSPAR: 2018-099. 1017LT SSO.

K2SAT - . Nation: Korea South. Type: Imaging/Com. Spacecraft: Cubesat. COSPAR: 2018-099. See K2SAT. Amateur radio cubesat for Korea AF Academy/KAIST. 1017LT SSO..

WeissSat 1 - . Nation: USA. Type: Tech. Spacecraft: Cubesat. COSPAR: 2018-099. See WeissSat 1. Technology 1U cubesat for Weiss School, Palm Beach, Florida. 1017LT SSO..

Exseedsat-1 (VO-96 - . Type: Comms. Spacecraft: Cubesat. COSPAR: 2018-099. See ExseedSat 1 (VO 96, VUsat-OSCAR 96). 1017LT SSO..

SeeMe - . Type: Imaging. Spacecraft: Cubesat. COSPAR: 2018-099. See SeeMe. 1017LT SSO..

Centauri 1 - . Type: Comms. Spacecraft: Cubesat. COSPAR: 2018-099. See Centauri 1. 1017LT SSO..

Audacy Zero - . Type: Comms. Spacecraft: Cubesat. COSPAR: 2018-099. See Audacy 0. Communications technology cubesat for Audacy/ClydeSpace. 1017LT SSO..

IRVINE02 - . Nation: USA. Type: Tech. Spacecraft: Cubesat. COSPAR: 2018-099.
See Irvine 02. Technology 1U cubesat for Irvine Public School Foundation, Irvine, California. 1U cubesat by Irvine CubeSat STEM Program. Mission: Test propulsion system and LED communications. Status as of 2019: Awaiting Launch. Built by high school students. Selected by NASA for CubeSat Launch Initiative. 1017LT SSO.

SIRION PF 2 - . Type: Comms. Spacecraft: Cubesat. COSPAR: 2018-099. See Sirion Pathfinder 2/Helios Wire Pathfinder 2. 1017LT SSO..

DoD Cube 2B - . Nation: USA. Type: Comms?. Spacecraft: Cubesat. COSPAR: 2018-099. 1017LT SSO.

Kodiak - . Nation: USA. Type: Comms. USAF Sat Cat: 43764 . COSPAR: 2018-099G. Apogee: 591 km (367 mi). Perigee: 567 km (352 mi). Inclination: 97.76 deg. Period: 96.25 min. See ORS 7B (Polar Scout 2, Kodiak). 1017LT SSO..

SeaHawk - . Type: Imaging. Spacecraft: Cubesat. COSPAR: 2018-099. See SeaHawk 1. 1017LT SSO..

ENOCH - . Nation: USA. Type: Art. Spacecraft: Cubesat. COSPAR: 2018-099. See Enoch. Art cubesat for LA County Mus. of Art, Tavares Strachan. 1017LT SSO..

THEA - . Nation: USA. Type: Sigint. Spacecraft: Cubesat. COSPAR: 2018-099. See THEA. Technology cubesat for Aurora Insight/DC, SpaceQuest. 1017LT SSO..

DoD Cube 2A - . Nation: USA. Type: Comms?. Spacecraft: Cubesat. COSPAR: 2018-099. 1017LT SSO.

VisionCube - . Nation: Korea South. Type: Atmos Sci. Spacecraft: Cubesat. COSPAR: 2018-099. See VisionCube. Specialized imaging cubesat for Korea Aerospace U. 1017LT SSO..

Hawk A - . Nation: USA. Type: Elint. USAF Sat Cat: 43765 . COSPAR: 2018-099H. Apogee: 591 km (367 mi). Perigee: 568 km (352 mi). Inclination: 97.76 deg. Period: 96.26 min. See Hawk A. 1017LT SSO..

Eaglet 1 - . Nation: TBD. Type: Imaging. USAF Sat Cat: 43790 . COSPAR: 2018-099AJ. Apogee: 591 km (367 mi). Perigee: 571 km (354 mi). Inclination: 97.76 deg. Period: 96.29 min. See Eaglet 1. 1017LT SSO..

Denali - . Nation: USA. Type: Radar. Spacecraft: Cubesat. USAF Sat Cat: 43791 . COSPAR: 2018-099AK. Apogee: 589 km (365 mi). Perigee: 572 km (355 mi). Inclination: 97.76 deg. Period: 96.29 min. See Capella 1 (Denali). Radar 12U cubesat for Capella Space. 1017LT SSO..

Landmapper-BC4 - . Nation: USA. Type: Imaging. Spacecraft: Cubesat. USAF Sat Cat: 43767 . COSPAR: 2018-099K. Apogee: 593 km (368 mi). Perigee: 575 km (357 mi). Inclination: 97.76 deg. Period: 96.35 min. See Landmapper-BC 4 (Corvus-BC 4). Imaging 6U cubesat for Astro Digital, San Jose/Mountain View. 1017LT SSO..

FalconSat-6 - . Nation: USA. Type: Tech. USAF Sat Cat: 43815 . COSPAR: 2018-099BK. Apogee: 593 km (368 mi). Perigee: 572 km (355 mi). Inclination: 97.76 deg. Period: 96.32 min. See FalconSat 6. 1017LT SSO..

SpaceBEE 7 - . Nation: USA. Type: Comms. USAF Sat Cat: 43816 . COSPAR: 2018-099BL. Apogee: 591 km (367 mi). Perigee: 572 km (355 mi). Inclination: 97.76 deg. Period: 96.30 min. See SpaceBEE 7. 1017LT SSO..

ESEO - . Nation: Europe. Type: Tech. USAF Sat Cat: 43792 . COSPAR: 2018-099AL. Apogee: 591 km (367 mi). Perigee: 571 km (354 mi). Inclination: 97.76 deg. Period: 96.29 min. See ESEO (FUNcube 4). 1017LT SSO..

AISTechSat-2 - . Nation: Spain. Type: Imaging/Com. Spacecraft: Cubesat. USAF Sat Cat: 43768 . COSPAR: 2018-099L. Apogee: 593 km (368 mi). Perigee: 575 km (357 mi). Inclination: 97.76 deg. Period: 96.36 min. See AISTECHSAT 2. AIS/ADS-B maritime/aviavtion location cubesat for AISTech, Barcelona (6U. 1017LT SSO..

CSIM-FD - . Nation: USA. Type: Tech. Spacecraft: Cubesat. USAF Sat Cat: 43793 . COSPAR: 2018-099AM. Apogee: 590 km (360 mi). Perigee: 571 km (354 mi). Inclination: 97.75 deg. Period: 96.29 min. See CSIM-FD. Astronomy 6U cubesat for U Colorado Boulder; solar irradiance. 1017LT SSO..

SpaceBEE 5 - . Nation: USA. Type: Comms. USAF Sat Cat: 43817 . COSPAR: 2018-099BM. Apogee: 591 km (367 mi). Perigee: 572 km (355 mi). Inclination: 97.76 deg. Period: 96.30 min. See SpaceBEE 5. 1017LT SSO..

Hawk B - . Nation: USA. Type: Elint. USAF Sat Cat: 43794 . COSPAR: 2018-099AN. Apogee: 591 km (367 mi). Perigee: 568 km (352 mi). Inclination: 97.76 deg. Period: 96.26 min. See Hawk B. 1017LT SSO..

Flock 3s-1 - . Payload: Dove 105C. Nation: USA. Type: Imaging. Spacecraft: Cubesat. USAF Sat Cat: 43770 . COSPAR: 2018-099N. Apogee: 594 km (369 mi). Perigee: 572 km (355 mi). Inclination: 97.76 deg. Period: 96.34 min. See Flock-3s 1 (Dove 105C). 1017LT SSO..

SpaceBEE 6 - . Nation: USA. Type: Comms. USAF Sat Cat: 43818 . COSPAR: 2018-099BN. Apogee: 591 km (367 mi). Perigee: 572 km (355 mi). Inclination: 97.76 deg. Period: 96.30 min. See SpaceBEE 6. 1017LT SSO..

Fox-1C (AO-95 - . Nation: USA. Type: Comms. USAF Sat Cat: 43770 . COSPAR: 2018-099N. Apogee: 594 km (369 mi). Perigee: 572 km (355 mi). Inclination: 97.76 deg. Period: 96.34 min. See Fox 1C (Fox 1Cliff, AO 95, AMSAT-OSCAR 95). 1017LT SSO..

eXCITe - . Nation: USA. Type: Tech. USAF Sat Cat: 43819 . COSPAR: 2018-099BP. Apogee: 592 km (367 mi). Perigee: 571 km (354 mi). Inclination: 97.76 deg. Period: 96.30 min. See eXCITe (PTB 1). 1017LT SSO..

Orbweaver 1 - . Nation: USA. Type: Tech. USAF Sat Cat: 43795 . COSPAR: 2018-099AP. Apogee: 591 km (367 mi). Perigee: 570 km (350 mi). Inclination: 97.75 deg. Period: 96.28 min. See OrbWeaver 1. 1017LT SSO..

RANGE A - . Nation: TBD. Type: Tech. USAF Sat Cat: 43772 . COSPAR: 2018-099Q. Apogee: 594 km (369 mi). Perigee: 573 km (356 mi). Inclination: 97.77 deg. Period: 96.34 min. See RANGE A. 1017LT SSO..

RANGE B - . Nation: USA. Type: Tech. USAF Sat Cat: 43773 . COSPAR: 2018-099R. Apogee: 593 km (368 mi). Perigee: 573 km (356 mi). Inclination: 97.76 deg. Period: 96.34 min. See RANGE B. 1017LT SSO..

Flock 3s-2 - . Payload: Dove 2151. Nation: USA. Type: Imaging. Spacecraft: Cubesat. USAF Sat Cat: 43821 . COSPAR: 2018-099BR. Apogee: 592 km (367 mi). Perigee: 571 km (354 mi). Inclination: 97.76 deg. Period: 96.30 min. See Flock-3s 2 (Dove 2151). 1017LT SSO..

SkySat C12 - . Nation: USA. Type: Imaging. USAF Sat Cat: 43797 . COSPAR: 2018-099AR. Apogee: 591 km (367 mi). Perigee: 570 km (350 mi). Inclination: 97.76 deg. Period: 96.28 min. See SkySat 14 (SkySat C12). 1017LT SSO..

Astrocast-0.1 - . Nation: Switzerland. Type: Comms. Spacecraft: Cubesat. COSPAR: 2018-099AS. See Astrocast 0.1. 1017LT SSO..

Hiber-2 - . Nation: Netherlands. Type: Comms. USAF Sat Cat: 43774 . COSPAR: 2018-099S. Apogee: 593 km (368 mi). Perigee: 573 km (356 mi). Inclination: 97.76 deg. Period: 96.33 min. See Hiber 2. 1017LT SSO..

Hawk C - . Nation: USA. Type: Elint. USAF Sat Cat: 43799 . COSPAR: 2018-099AT. Apogee: 591 km (367 mi). Perigee: 568 km (352 mi). Inclination: 97.76 deg. Period: 96.26 min. See Hawk C. 1017LT SSO..

SkySat C13 - . Nation: USA. Type: Imaging. USAF Sat Cat: 43802 . COSPAR: 2018-099AW. Apogee: 576 km (357 mi). Perigee: 563 km (349 mi). Inclination: 97.75 deg. Period: 96.05 min. See SkySat 15 (SkySat C13). 1017LT SSO..

JY1SAT (JO-97 - . Nation: Jordan. Type: Comms. USAF Sat Cat: 43803 . COSPAR: 2018-099AX. Apogee: 593 km (368 mi). Perigee: 571 km (354 mi). Inclination: 97.76 deg. Period: 96.31 min. See JY1-Sat (FUNcube 6, JO 97, Jordan-OSCAR 97). 1017LT SSO..

MOVE 2 - . Nation: Germany. Type: Tech. USAF Sat Cat: 43780 . COSPAR: 2018-099Y. Apogee: 593 km (368 mi). Perigee: 572 km (355 mi). Inclination: 97.76 deg. Period: 96.33 min. See MOVE 2. 1017LT SSO..

Suomi-100 - . Nation: Finland. Type: Tech. Spacecraft: Cubesat. USAF Sat Cat: 43804 . COSPAR: 2018-099AY. Apogee: 593 km (368 mi). Perigee: 570 km (350 mi). Inclination: 97.76 deg. Period: 96.31 min. See Suomi-100. Technology 1U cubesat for Aalto U. 1017LT SSO..

VESTA - . Nation: UK. Type: Comms. Spacecraft: Cubesat. USAF Sat Cat: 43781 . COSPAR: 2018-099Z. Apogee: 593 km (368 mi). Perigee: 572 km (355 mi). Inclination: 97.75 deg. Period: 96.33 min. See VESTA. AIS/ADS-B maritime/aviavtion location cubesat for Surrey/UKSA. 1017LT SSO..

Al Farabi 2 - . Nation: TBD. Type: Comms. USAF Sat Cat: 43805 . COSPAR: 2018-099AZ. Apogee: 593 km (368 mi). Perigee: 570 km (350 mi). Inclination: 97.76 deg. Period: 96.31 min. See Al-Farabi 2. 1017LT SSO..

SNUSAT 2 - . Nation: Korea South. Type: Imaging. Spacecraft: Cubesat. USAF Sat Cat: 43782 . COSPAR: 2018-099AA. Apogee: 592 km (367 mi). Perigee: 573 km (356 mi). Inclination: 97.76 deg. Period: 96.32 min. See SNUSAT 2. Imaging cubesat for Seoul Natl. U. 1017LT SSO..

Eu:CROPIS - . Nation: Germany. Type: Rem.Sensing. USAF Sat Cat: 43807 . COSPAR: 2018-099BB. Apogee: 591 km (367 mi). Perigee: 572 km (355 mi). Inclination: 97.76 deg. Period: 96.30 min. See Eu:CROPIS. 1017LT SSO..

KazSTSat - . Nation: Kazakhstan. Type: Imaging. USAF Sat Cat: 43783 . COSPAR: 2018-099AB. Apogee: 594 km (369 mi). Perigee: 580 km (360 mi). Inclination: 97.77 deg. Period: 96.41 min. See KazSTSAT. 1017LT SSO..

KazSciSat - . Nation: Kazakhstan. Type: Tech. Spacecraft: Cubesat. USAF Sat Cat: 43783 . COSPAR: 2018-099AB. Apogee: 594 km (369 mi). Perigee: 580 km (360 mi). Inclination: 97.77 deg. Period: 96.41 min. See KazSTSAT. Technology cubesat for Ghalam LLP, Astana. 1017LT SSO..

Yukon - . Nation: USA. Type: Comms. USAF Sat Cat: 43808 . COSPAR: 2018-099BC. Apogee: 591 km (367 mi). Perigee: 572 km (355 mi). Inclination: 97.76 deg. Period: 96.30 min. See ORS 7A (Polar Scout 1, Yukon). 1017LT SSO..

SNUGLITE - . Nation: Korea South. Type: Tech/Comms. Spacecraft: Cubesat. USAF Sat Cat: 43784 . COSPAR: 2018-099AC. Apogee: 594 km (369 mi). Perigee: 571 km (354 mi). Inclination: 97.76 deg. Period: 96.32 min. See SNUGLITE. Amateur radio cubesat for Seoul Natl. U. 1017LT SSO..

Orbweaver 2 - . Nation: USA. Type: Tech. USAF Sat Cat: 43785 . COSPAR: 2018-099AD. Apogee: 592 km (367 mi). Perigee: 572 km (355 mi). Inclination: 97.75 deg. Period: 96.32 min. See OrbWeaver 2. 1017LT SSO..

ITASAT-1 - . Nation: TBD. Type: Tech. USAF Sat Cat: 43786 . COSPAR: 2018-099AE. Apogee: 594 km (369 mi). Perigee: 571 km (354 mi). Inclination: 97.76 deg. Period: 96.32 min. See ITASAT 1. 1017LT SSO..

NEXTSat-1 - . Nation: Korea South. Type: IR Astron. USAF Sat Cat: 43811 . COSPAR: 2018-099BF. Apogee: 591 km (367 mi). Perigee: 572 km (355 mi). Inclination: 97.76 deg. Period: 96.30 min. See NEXTSat 1. 1017LT SSO..

Flock 3s-3 - . Payload: Dove 210D. Nation: USA. Type: Imaging. Spacecraft: Cubesat. USAF Sat Cat: 43788 . COSPAR: 2018-099AG. Apogee: 593 km (368 mi). Perigee: 571 km (354 mi). Inclination: 97.76 deg. Period: 96.31 min. See Flock-3s 3 (Dove 210D). 1017LT SSO..

Global-2 - . Nation: USA. Type: Imaging. USAF Sat Cat: 43812 . COSPAR: 2018-099BG. Apogee: 592 km (367 mi). Perigee: 571 km (354 mi). Inclination: 97.76 deg. Period: 96.30 min. See BlackSky Global 2. 1017LT SSO..

BRIO - . Type: Tech. Spacecraft: Cubesat. COSPAR: 2018-099BH. See BRIO. Communications technology cubesat for SpaceQuest/Myriota. 1017LT SSO..

PW-Sat 2 - . Nation: Poland. Type: Tech. USAF Sat Cat: 43814 . COSPAR: 2018-099BJ. Apogee: 584 km (362 mi). Perigee: 576 km (357 mi). Inclination: 97.77 deg. Period: 96.27 min. See PW-Sat 2. 1017LT SSO..

2018 December 5 - . 18:15 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral SLC40. LV Family: Falcon. Launch Vehicle: Falcon 9.

Dragon CRS-16 - . Nation: USA. Program: ISS. Class: Manned. Type: Manned logistics spacecraft. Spacecraft: Dragon. USAF Sat Cat: 43827 . COSPAR: 2018-101A. Apogee: 405 km (251 mi). Perigee: 395 km (245 mi). Inclination: 51.64 deg. Period: 92.56 min. See Dragon CRS-16 (SpX 16, Dragon C112-F2). ..

2018 December 23 - . 13:50 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral SLC40. LV Family: Falcon. Launch Vehicle: Falcon 9.

GPS III SV01 - . Nation: USA. Type: Navigation 1. USAF Sat Cat: 43873 . COSPAR: 2018-109A. Apogee: 20,196 km (12,549 mi). Perigee: 20,167 km (12,531 mi). Inclination: 55.00 deg. Period: 717.94 min. See GPS-3 1 (Navstar 74, USA 289, Vespucci). ..

2019 January 11 - . 15:30 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg SLC4E. LV Family: Falcon. Launch Vehicle: Falcon 9.

Iridium SV180 - . Nation: USA. Type: Comms 0. USAF Sat Cat: 43922 . COSPAR: 2019-002A. Apogee: 779 km (484 mi). Perigee: 777 km (482 mi). Inclination: 86.40 deg. Period: 100.40 min. See Iridium-NEXT 167. ..

Iridium SV176 - . Nation: USA. Type: Comms 0. USAF Sat Cat: 43923 . COSPAR: 2019-002B. Apogee: 656 km (407 mi). Perigee: 652 km (405 mi). Inclination: 86.61 deg. Period: 97.81 min. See Iridium-NEXT 176. ..

Iridium SV168 - . Nation: USA. Type: Comms 0. USAF Sat Cat: 43924 . COSPAR: 2019-002C. Apogee: 779 km (484 mi). Perigee: 776 km (482 mi). Inclination: 86.40 deg. Period: 100.40 min. See Iridium-NEXT 168. ..

Iridium SV173 - . Nation: USA. Type: Comms 0. USAF Sat Cat: 43925 . COSPAR: 2019-002D. Apogee: 779 km (484 mi). Perigee: 776 km (482 mi). Inclination: 86.40 deg. Period: 100.40 min. See Iridium-NEXT 173. ..

Iridium SV169 - . Nation: USA. Type: Comms 0. USAF Sat Cat: 43926 . COSPAR: 2019-002E. Apogee: 702 km (436 mi). Perigee: 698 km (433 mi). Inclination: 87.03 deg. Period: 98.77 min. See Iridium-NEXT 169. ..

Iridium SV172 - . Nation: USA. Type: Comms 0. USAF Sat Cat: 43927 . COSPAR: 2019-002F. Apogee: 779 km (484 mi). Perigee: 776 km (482 mi). Inclination: 86.40 deg. Period: 100.40 min. See Iridium-NEXT 172. ..

Iridium SV175 - . Nation: USA. Type: Comms 0. USAF Sat Cat: 43928 . COSPAR: 2019-002G. Apogee: 656 km (407 mi). Perigee: 652 km (405 mi). Inclination: 86.61 deg. Period: 97.81 min. See Iridium-NEXT 175. ..

Iridium SV171 - . Nation: USA. Type: Comms 0. USAF Sat Cat: 43929 . COSPAR: 2019-002H. Apogee: 779 km (484 mi). Perigee: 776 km (482 mi). Inclination: 86.40 deg. Period: 100.40 min. See Iridium-NEXT 171. ..

Iridium SV170 - . Nation: USA. Type: Comms 0. USAF Sat Cat: 43930 . COSPAR: 2019-002J. Apogee: 629 km (390 mi). Perigee: 608 km (377 mi). Inclination: 86.68 deg. Period: 97.07 min. See Iridium-NEXT 170. ..

Iridium SV167 - . Nation: USA. Type: Comms 0. USAF Sat Cat: 43931 . COSPAR: 2019-002K. Apogee: 779 km (484 mi). Perigee: 777 km (482 mi). Inclination: 86.40 deg. Period: 100.40 min. See Iridium-NEXT 167. ..

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