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Sriharikota PSLV

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AKA: Sriharikota FLP;Sriharikota LP1. First Launch: 1993-09-20. Last Launch: 2014-06-30. Number: 24 . Longitude: 80.23 deg. Latitude: 13.73 deg.

• IRS-1E - . Payload: IRS-1E. Mass: 1,250 kg (2,750 lb). Nation: India. Agency: ISRO. Class: Earth. Type: Earth resources satellite. Spacecraft: IRS.

• IRS-P2 - . Mass: 870 kg (1,910 lb). Nation: India. Agency: ISRO. Class: Earth. Type: Earth resources satellite. Spacecraft: IRS. USAF Sat Cat: 23323 . COSPAR: 1994-068A. Apogee: 820 km (500 mi). Perigee: 818 km (508 mi). Inclination: 98.67 deg. Period: 101.29 min. Remote sensing; sun-synch orbit..

• IRS-P3 - . Mass: 930 kg (2,050 lb). Nation: India. Agency: ISRO. Class: Earth. Type: Earth resources satellite. Spacecraft: IRS. USAF Sat Cat: 23827 . COSPAR: 1996-017A. Apogee: 820 km (500 mi). Perigee: 819 km (508 mi). Inclination: 98.50 deg. Period: 101.30 min. LEO .

• IRS-1D - . Payload: IRS-P3. Mass: 1,250 kg (2,750 lb). Nation: India. Agency: ISRO. Class: Earth. Type: Earth resources satellite. Spacecraft: IRS. USAF Sat Cat: 24971 . COSPAR: 1997-057A. Apogee: 823 km (511 mi). Perigee: 742 km (461 mi). Inclination: 98.50 deg. Period: 100.50 min.

• Kitsat-3 - . Mass: 50 kg (110 lb). Nation: Korea South. Agency: ISRO. Manufacturer: KAIST. Class: Earth. Type: Seismology satellite. Spacecraft: Kitsat. USAF Sat Cat: 25756 . COSPAR: 1999-029A. Apogee: 727 km (451 mi). Perigee: 707 km (439 mi). Inclination: 98.60 deg. Period: 99.10 min.

• OceanSat 1 (IRS-P4) - . Payload: IRS-P4. Mass: 1,036 kg (2,283 lb). Nation: India. Agency: ISRO. Class: Earth. Type: Sea satellite. Spacecraft: IRS. USAF Sat Cat: 25758 . COSPAR: 1999-029C. Apogee: 724 km (449 mi). Perigee: 721 km (448 mi). Inclination: 98.30 deg. Period: 99.30 min. Remote sensing satellite with Ocean Colour Monitor (OCM) and a Multi-frequency Scanning Microwave Radiometer (MSMR).

• DLR-Tubsat - . Mass: 45 kg (99 lb). Nation: Germany. Agency: DLR. Class: Earth. Type: Seismology satellite. Spacecraft: Tubsat. USAF Sat Cat: 25757 . COSPAR: 1999-029B. Apogee: 733 km (455 mi). Perigee: 712 km (442 mi). Inclination: 98.60 deg. Period: 99.20 min.

  DLR-Tubsat carried on the experimental work of Tubsat-A and -B. The satellite measured 32x32x32 cm and had a mass of 44.8 kg. The dechnology demonstrator conducted earth observation with 6 m resolution and conducted attitude control experiments. It was still in operation as of 2003.

• GSAT-1 - . Payload: GramSat. Mass: 1,530 kg (3,370 lb). Nation: India. Agency: ISRO. Program: Insat. Class: Communications. Type: Civilian communications satellite. Spacecraft: I-2K. USAF Sat Cat: 26745 . COSPAR: 2001-015A. Apogee: 35,814 km (22,253 mi). Perigee: 33,825 km (21,017 mi). Inclination: 0.00 deg. Period: 1,387.00 min.

  Experimental Rural Communications satellite. Launch delayed following pad abort on March 28. First launch of the Indian GSLV launch vehicle. GSat 1 was an Indian, 1500 kg scaled-dow) test model of a future geosynchronous communications spacecraft with a 440 N ISRO liquid apogee motor, and S-band and C-band ommunications transponders, similar to the Insat-2 satellites. The motor for the cryogenic, hydrogen-oxygen upper stage had been purchased from Russia but the design had never flown in space before. The stage cut off without providing the required delta-V - preliminary analysis revealed a shortfall of 0.5% in the thrust. An attempt was made to reach a usable orbit using the station-keeping motor of the GSAT satellite itself. After a series of burns, GSat 1 ran out of propellant - 10 kg more fuel would have been required to reach a stationary orbit. In the end, the parameters of the drifting (about 13 deg/day) orbit were period 23 hours, apogee 35,665 km, perigee 33,806 km, and inclination 0.99 deg. The fully functional transponders and transmitters on board were deactivated on instructions of the International Telecommunications Union. As of 4 September 2001 located at 54.88 deg E drifting at 13.212 deg E per day. As of 2007 Mar 10 located at 50.16W drifting at 12.778E degrees per day.

• TES - . Mass: 1,108 kg (2,442 lb). Nation: India. Agency: ISRO. Class: Surveillance. Type: Military surveillance satellite. Spacecraft Bus: IRS. Spacecraft: TES. USAF Sat Cat: 26957 . COSPAR: 2001-049A. Apogee: 592 km (367 mi). Perigee: 533 km (331 mi). Inclination: 97.60 deg. Period: 95.90 min.

  Launch delayed from July 20. The PS4 upper stage deployed the 1108 kg Indian TES (Technology Experiment Satellite) into a sun-synchronous orbit at 05:09:10 GMT. TES was an imaging satellite equipped with cameras and instruments to test military reconnaissance satellite technology. It was probably based on the IRS remote sensing satellite and carried a one-meter resolution panchromatic camera. India decided to develop an independent indigenous reconnaissance satellite capability after the 1999 incursion of Pakistani troops into disputed territory in Kashmir caught it by surprise. TES was developed by ISRO, the Indian Space Research Organization.

• BIRD - . Mass: 1,108 kg (2,442 lb). Nation: Germany. Agency: ISRO. Class: Earth. Type: Earth resources satellite. Spacecraft: BIRD. USAF Sat Cat: 26959 . COSPAR: 2001-049C. Apogee: 529 km (328 mi). Perigee: 509 km (316 mi). Inclination: 97.90 deg. Period: 95.00 min.

  BIRD (Bispectral IR Detector) was a 94 kg German research minisatellite testing a new sensor for Earth imaging studies, detecting forest fires and other hot spots and studying vegetation changes. BIRD was released by the PS4 upper stage 40 seconds after the primary TES satellite payload had been deployed. The technology demonstrator was to help in the design a major remote sensing array of infrared detectors.

• PROBA - . Mass: 1,108 kg (2,442 lb). Nation: Europe. Agency: ISRO. Class: Earth. Type: Earth resources satellite. Spacecraft: PROBA. USAF Sat Cat: 26958 . COSPAR: 2001-049B. Apogee: 677 km (420 mi). Perigee: 553 km (343 mi). Inclination: 97.90 deg.

  Proba (PRoject for On-Board Autonomy, 1) was a European Space Agency technology development minisatellite with a mass of 94 kg. It carried a radiation detector, an IR spectrometer, debris impact detectors, Earth imaging cameras, and an experimental spacecraft processor for spacecraft autonomy experiments. The satellite was built by Verheart in Belgium using the MiniSIL bus developed by SI of England, and was controlled from Belgium. After release of the TES and BIRD satellites, the PS4's upper stage small RCS engines raised the orbit to 553 x 676 km, and PROBA was ejected at 0520 GMT.

• Metsat 1 - . Mass: 1,000 kg (2,200 lb). Nation: Europe. Agency: ISRO. Class: Earth. Type: Weather satellite. Spacecraft: I-1K. USAF Sat Cat: 27525 . COSPAR: 2002-043A. Apogee: 35,809 km (22,250 mi). Perigee: 35,764 km (22,222 mi). Inclination: 0.30 deg. Period: 1,436.10 min.

  METSAT 1 was an Indian (ISRO) meteorological, geostationary satellite that was launched by an upgraded, four-stage PSLV-C4 rocket. The satellite was manoeuvred from the transfer orbit to a geostationary postion at 37° E longitude on September 16, and then was parked at 74° E longitude on September 24. As of 2007 Mar 11 located at 74.00E drifting at 0.007W degrees per day.

• GSAT-2 - . Payload: GramSat. Mass: 1,825 kg (4,023 lb). Nation: India. Agency: ISRO. Program: Insat. Class: Communications. Type: Civilian communications satellite. Spacecraft: I-2K. USAF Sat Cat: 27807 . COSPAR: 2003-018A. Apogee: 35,790 km (22,230 mi). Perigee: 35,782 km (22,233 mi). Inclination: 0.00 deg. Period: 1,436.10 min.

  Experimental Rural Communications. Launch delayed from original target of late 2001, then October 2002, then February 2003. The satellite carried four C-band transponders, two Ku-band transponders and a Mobile Satellite Service (MSS) payload operating in S-band and C-band for forward link and return link respectively. GSAT-2 also carried four piggyback experimental payloads: Total Radiation Dose Monitor (TRDM), Surface Charge Monitor (SCM), Solar X-ray Spectrometer (SOXS) and Coherent Radio Beacon Experiment (CRABEX). As of 2007 Mar 10 located at 47.97E drifting at 0.005E degrees per day.

• ResourceSat 1 (IRS-P6) - . Mass: 1,360 kg (2,990 lb). Nation: India. Agency: ISRO. Program: IRS. Class: Earth. Type: Earth resources satellite. Spacecraft: IRS. USAF Sat Cat: 28051 . COSPAR: 2003-046A. Apogee: 836 km (519 mi). Perigee: 813 km (505 mi). Inclination: 98.80 deg. Period: 101.40 min. The satellite was to replace IRS-1C and IRS-1D, and carried three cameras for remote sensing, the highest resolution one being the 6-meter LISS-4 imager. The sensors were designed for agricultural remote sensing applications..

• GSAT-3 / Edusat - . Payload: GramSat. Mass: 1,950 kg (4,290 lb). Nation: India. Agency: ISRO. Program: Insat. Class: Communications. Type: Civilian communications satellite. Spacecraft: I-2K. USAF Sat Cat: 28417 . COSPAR: 2004-036A. Apogee: 35,801 km (22,245 mi). Perigee: 35,772 km (22,227 mi). Inclination: 0.10 deg. Period: 1,436.10 min.

  Gsat-3 / Edusat was the first Indian satellite built exclusively for the educational sector. It was mainly intended to meet the demand for an interactive satellite based distance education system for India. Edusat was launched into a geosynchronous transfer orbit by its launch vehicle. Edusat was to reach geostationary orbit by firing, in stages, its on board Liquid Apogee Motor (LAM). In geostationary orbit the satellite was to be co-located with Kalpana-1 and Insat-3C satellites at 74 deg East longitude.

  Compared to earlier satellites in the Insat series, Edusat used several new technologies. The spacecraft was built around the I-2K standardised spacecraft bus. It had a multiple spot beam antenna with a 1.2 m reflector to direct Ku band spot beams, a dual core bent heat pipe for thermal control, high efficiency multi-junction solar cells and an improved thruster configuration for optimised propellant use for orbit and orientation maintenance. The satellite used radiatively cooled Ku-band Travelling Wave Tube Amplifiers and a dielectrically loaded C-band demultiplexer for its communication payloads. Edusat carried five Ku-band transponders providing spot beams, one Ku-band transponder providing a national beam and six Extended C-band transponders with a national coverage beam. It was to join the Insat system that already provided more than 130 transponders in C-band, Extended C-band and Ku-band for a variety of telecommunication and television services.

  First operational flight of launch vehicle. Launch delayed from July, August and September 10. Dry mass 820 kg. As of 2007 Mar 9 located at 73.92E drifting at 0.006W degrees per day.

• SRE-1 - . Mass: 550 kg (1,210 lb). Nation: India. Agency: ISRO. Class: Technology. Type: Re-entry test vehicle. Spacecraft: SRE. Decay Date: 2007-01-22 . USAF Sat Cat: 29711 . COSPAR: 2007-001C. Apogee: 643 km (399 mi). Perigee: 620 km (380 mi). Inclination: 97.90 deg. Period: 97.40 min.

  India's Space Recovery Experiment-1 India's SRE-1 first lowered to its orbit to 485 km x 643 km on January 20. A 10-minute deorbit burn began at 03:30 GMT on January 22, with re-entry beginning at 04:07 and a successful splashdown at 04:16 GMT in the Bay of Bengal near 13.3 N / 81.4E. The capsule was successfully recovered by the Indian Navy. The capsule returned two microgravity payloads as well as proving basic technologies for any eventual Indian manned space program. It was also announced that the capsule could be used to orbit further microgravity payloads at low cost to customers.

• LAPAN Tubsat - . Mass: 56 kg (123 lb). Nation: Indonesia. Agency: ISRO. Class: Technology. Type: Navigation technology satellite. Spacecraft: Tubsat. USAF Sat Cat: 29709 . COSPAR: 2007-001A. Apogee: 638 km (396 mi). Perigee: 620 km (380 mi). Inclination: 97.90 deg. Period: 97.30 min. Experimental satellite developed with assistance from TUB (Berlin Technical University. It carried a 5-meter-resolution surveillance camera..

• Cartosat-2 - . Mass: 680 kg (1,490 lb). Nation: India. Agency: ISRO. Class: Surveillance. Type: Civilian surveillance satellite. Spacecraft: IRS. USAF Sat Cat: 29710 . COSPAR: 2007-001B. Apogee: 644 km (400 mi). Perigee: 629 km (390 mi). Inclination: 98.00 deg. Period: 97.40 min.

  The satellite was the twelfth in the Indian Remote Sensing satellite series and was capable of providing scene-specific spot imagery. The panchromatic camera provided imagery with a spatial resolution of better than one metre and a swath of 9.6 km. Data from the satellite was to be used for detailed mapping.

• Pehuensat - . Mass: 6.00 kg (13.20 lb). Nation: Argentina. Agency: ISRO. Class: Technology. Type: Navigation technology satellite. Spacecraft: Pehuensat. USAF Sat Cat: 29712 . COSPAR: 2007-001D. Apogee: 641 km (398 mi). Perigee: 621 km (385 mi). Inclination: 97.90 deg. Period: 97.30 min. Experimental satellite developed by the Universidad Nacional del Comahue and AMSAT-LU. The satellte remained attached to the PSLV's Dual Launch Adapter..

• Oceansat-2 - . Mass: 1,000 kg (2,200 lb). Nation: India. Agency: ISRO. Class: Surveillance. Type: Surveillance satellite. Spacecraft Bus: IRS. Spacecraft: Oceansat. USAF Sat Cat: 35931 . COSPAR: 2009-051A. Apogee: 726 km (451 mi). Perigee: 720 km (440 mi). Inclination: 98.30 deg. Period: 99.20 min. Remote sensing satellite with an 8-band ocean color monitor, a radar scatterometer and a radio occultation atmospheric sounder..

• SwissCube - . Mass: 1.00 kg (2.20 lb). Nation: India. Class: Science. Type: Science satellite. Spacecraft: Cubesat. USAF Sat Cat: 35932 . COSPAR: 2009-051B. Apogee: 712 km (442 mi). Perigee: 702 km (436 mi). Inclination: 98.43 deg. Period: 98.93 min. Cubesat from Ecole Polytechnique Federale de Lausanne, Switzerland.

• BEESAT - . Mass: 1.00 kg (2.20 lb). Nation: India. Class: Technology. Type: Technology satellite. Spacecraft: Cubesat. USAF Sat Cat: 35933 . COSPAR: 2009-051C. Apogee: 710 km (440 mi). Perigee: 703 km (436 mi). Inclination: 98.43 deg. Period: 98.92 min. Cubesat from Technische Universitat Berlin, Germany..

• UWE-2 - . Mass: 1.00 kg (2.20 lb). Nation: India. Class: Technology. Type: Technology satellite. Spacecraft: Cubesat. USAF Sat Cat: 35934 . COSPAR: 2009-051D. Apogee: 712 km (442 mi). Perigee: 704 km (437 mi). Inclination: 98.42 deg. Period: 98.95 min. 1U cubesat from Julius-Maximilians-Universitat Wurzburg, Germany. ADCS technology demonstrator. Successful..

• ITU-p-SAT 1 - . Mass: 1.00 kg (2.20 lb). Nation: India. Class: Technology. Type: Technology satellite. Spacecraft: Cubesat. USAF Sat Cat: 35935 . COSPAR: 2009-051E. Apogee: 715 km (444 mi). Perigee: 704 km (437 mi). Inclination: 98.44 deg. Period: 98.97 min. Cubesat from Istanbul Teknik Universitesi..

• Rubin-9.1 - . Nation: India. Agency: ISRO. Class: Communications. Type: Civilian communications satellite. Spacecraft: Rubin. USAF Sat Cat: 35936 . COSPAR: 2009-051F. Apogee: 795 km (493 mi). Perigee: 715 km (444 mi). Inclination: 98.30 deg. Period: 99.90 min. Maritime communications package which remained attached to the PSLV final stage..

• Rubin-9.2 - . Nation: India. Agency: ISRO. Class: Communications. Type: Civilian communications satellite. Spacecraft: Rubin. USAF Sat Cat: 35936 . COSPAR: 2009-051F. Apogee: 795 km (493 mi). Perigee: 715 km (444 mi). Inclination: 98.30 deg. Period: 99.90 min. Maritime communications package which remained attached to the PSLV final stage..

• Cartosat 2B - . Mass: 694 kg (1,530 lb). Nation: India. Agency: ISRO. Class: Surveillance. Type: Cartographic satellite. Spacecraft: IRS. USAF Sat Cat: 36795 . COSPAR: 2010-035A. Apogee: 647 km (402 mi). Perigee: 629 km (390 mi). Inclination: 98.10 deg. Period: 97.50 min. Cartography satellite with 0.8 meter resolution..

• Studsat - . Mass: 1.00 kg (2.20 lb). Nation: India. Agency: ISRO. Class: Technology. Type: Technology satellite. Spacecraft: Cubesat. USAF Sat Cat: 36796 . COSPAR: 2010-035B. Apogee: 640 km (390 mi). Perigee: 621 km (385 mi). Inclination: 98.20 deg. Period: 97.30 min. ISRO-sponsored Indian student-designed 1U cubesat. First Indian picosatellite..

• Aissat 1 - . Mass: 6.00 kg (13.20 lb). Nation: Norway. Agency: ISRO. Program: AIS. Class: Navigation. Type: Navigation satellite. Spacecraft: Toronto GNB. USAF Sat Cat: 36797 . COSPAR: 2010-035C. Apogee: 636 km (395 mi). Perigee: 620 km (380 mi). Inclination: 98.20 deg. Period: 97.30 min. Satellite-based Automatic Identification System (AIS) payload to track maritime assets worldwide (all vessels over 300 metric tons are equipped with AIS transponders)..

• Alsat 2A - . Mass: 116 kg (255 lb). Nation: Algeria. Agency: ISRO. Program: Alsat. Class: Surveillance. Type: SIGINT. Spacecraft: Myriade. USAF Sat Cat: 36798 . COSPAR: 2010-035D. Apogee: 674 km (418 mi). Perigee: 672 km (417 mi). Inclination: 98.20 deg. Period: 98.20 min. Optical surveillance satellite with 2.5 meter panchromatic resolution and 10 meter in 4 band/multispectral mode..

• Tisat 1 - . Mass: 1.00 kg (2.20 lb). Nation: Switzerland. Agency: ISRO. Class: Technology. Type: Technology satellite. Spacecraft: Cubesat. USAF Sat Cat: 36799 . COSPAR: 2010-035E. Apogee: 639 km (397 mi). Perigee: 619 km (384 mi). Inclination: 98.20 deg. Period: 97.30 min. Swiss student 1U cubesat for SUPSI. Successful..

• Resourcesat 2 - . Mass: 1,200 kg (2,600 lb). Nation: India. Program: IRS. Class: Surveillance. Type: Military surveillance satellite. Spacecraft: IRS. USAF Sat Cat: 37387 . COSPAR: 2011-015A. Apogee: 825 km (512 mi). Perigee: 820 km (500 mi). Inclination: 98.80 deg. Period: 101.30 min.

  Surveillance satellite. Carried the LISS-4 camera, a 6-meter-resolution imager, which was to be used for both military reconnaissance and civilian remote sensing. It also carried the lower resolution LISS-3 (23 m resolution) and AWIFS (56 m resolution), and an AIS Automatic Identification System payload for Comdev of Canada for tracking ships at sea.

• Youthsat - . Mass: 92 kg (202 lb). Nation: India. Class: Science. Type: Science satellite. Spacecraft: Youthsat. USAF Sat Cat: 37388 . COSPAR: 2011-015B. Apogee: 823 km (511 mi). Perigee: 803 km (498 mi). Inclination: 98.80 deg. Period: 101.20 min. Joint Indian-Russian student satellite. Carried experiments to study solar-terrestrial relationships..

• X-Sat - . Mass: 105 kg (231 lb). Nation: India. Class: Earth. Type: Earth resources satellite. Spacecraft Bus: SI-100. Spacecraft: X-Sat. USAF Sat Cat: 37389 . COSPAR: 2011-015C. Apogee: 822 km (510 mi). Perigee: 803 km (498 mi). Inclination: 98.80 deg. Period: 101.10 min. Nanyang Technological University Singapore satellite; carried a 10-meter-resolution multispectral imager..

• GSAT-12 - . Mass: 1,410 kg (3,100 lb). Nation: India. Program: Insat. Class: Communications. Type: Civilian communications satellite. Spacecraft: I-1K. USAF Sat Cat: 37746 . COSPAR: 2011-034A. Apogee: 35,806 km (22,248 mi). Perigee: 35,768 km (22,225 mi). Inclination: 0.10 deg. Period: 1,436.10 min. Communications satellite; used on-board propellant to reach geosynchronous position..

• Megha-Tropique - . Mass: 1,000 kg (2,200 lb). Nation: India. Class: Earth. Type: Earth resources satellite. Spacecraft: IRS. USAF Sat Cat: 37838 . COSPAR: 2011-058A. Apogee: 868 km (539 mi). Perigee: 853 km (530 mi). Inclination: 20.00 deg. Period: 102.20 min. Joint Indian-French remote sensing satellite; carried a MADRAS microwave imager, a Saphir water vapor profile instrument, and a ScaRaB radiation budget scanner..

• JUGNU - . Mass: 10 kg (22 lb). Nation: India. Class: Technology. Type: Technology satellite. Spacecraft: Cubesat. USAF Sat Cat: 37839 . COSPAR: 2011-058B. Apogee: 866 km (538 mi). Perigee: 839 km (521 mi). Inclination: 20.00 deg. Period: 102.00 min. 3U cubesat for the Indian Institute of Technology in Kanpur. Micro-imaging system, near infrared camera to observe vegetation, and GPS Receiver to aid tracking. Successful..

• Vesselsat 1 - . Mass: 29 kg (63 lb). Nation: Luxembourg. Class: Technology. Type: Technology satellite. Spacecraft: Vesselsat. USAF Sat Cat: 37840 . COSPAR: 2011-058C. Apogee: 868 km (539 mi). Perigee: 847 km (526 mi). Inclination: 20.00 deg. Period: 102.10 min. OHB LuxSpace of Luxembourg satllite to provide AIS (ship tracking) services for Orbcomm..

• SRMSAT - . Mass: 10 kg (22 lb). Nation: India. Class: Earth. Type: Climate satellite. Spacecraft: SRMSAT. USAF Sat Cat: 37841 . COSPAR: 2011-058D. Apogee: 868 km (539 mi). Perigee: 850 km (520 mi). Inclination: 20.00 deg. Period: 102.10 min. SRM University in Chennai satellite for greenhouse gas monitoring..

• RISAT-1 - . Mass: 1,858 kg (4,096 lb). Nation: India. Class: Surveillance. Type: Civilian Radarsat. Spacecraft: IRS. USAF Sat Cat: 38248 . COSPAR: 2012-017A. Apogee: 550 km (340 mi). Perigee: 529 km (328 mi). Inclination: 97.60 deg. Period: 95.40 min. Radar Imaging Satellite with a C-band synthetic aperture radar payload mounted on an IRS- derived bus..

• Spot 6 - . Mass: 712 kg (1,569 lb). Nation: France. Class: Earth. Type: Earth resources satellite. Spacecraft: Astrobus. USAF Sat Cat: 38755 . COSPAR: 2012-047A. Apogee: 699 km (434 mi). Perigee: 697 km (433 mi). Inclination: 98.20 deg. Period: 98.70 min. Earth observing satellite built by Astrium/Toulouse for Astrium subsidiary Spot Image (Toulouse)..

• Proiteres - . Mass: 15 kg (33 lb). Nation: Japan. Class: Technology. Type: Ion engine technology satellite. Spacecraft: Cubesat. USAF Sat Cat: 38756 . COSPAR: 2012-047B. Apogee: 657 km (408 mi). Perigee: 640 km (390 mi). Inclination: 98.30 deg. Period: 97.70 min. 15 kg pulsed plasma thruster experiment: 'Project of Osaka Institute of Technology Electric Rocket Engine aboard small Spaceship'..

• AAUSAT3 - . Mass: 1.00 kg (2.20 lb). Nation: Denmark. Class: Navigation. Type: Navigation satellite. Spacecraft: Cubesat. USAF Sat Cat: 39087 . COSPAR: 2013-009B. Apogee: 787 km (489 mi). Perigee: 770 km (470 mi). Inclination: 98.63 deg. Period: 100.41 min. 2U cubesat built by Aalborg University in Denmark; carried a double AIS ship tracking receiver and a GPS receiver for tracking ships in Arctic regions. Successful..

• NEOSSat - . Mass: 65 kg (143 lb). Nation: Canada. Class: Astronomy. Type: Astronomy satellite. Spacecraft: Multi-Mission Microsatellite Bus. USAF Sat Cat: 39089 . COSPAR: 2013-009D. Apogee: 786 km (488 mi). Perigee: 771 km (479 mi). Inclination: 98.63 deg. Period: 100.43 min. Near Earth Object Surveillance Satellite, joint Canadian Space Agency/DRDC mission to survey asteroids and space debris, also with a 0.15m telescope..

• STRaND-1 - . Mass: 4.00 kg (8.80 lb). Nation: UK. Agency: Surrey. Manufacturer: Surrey. Class: Technology. Type: Technology satellite. Spacecraft: Cubesat. USAF Sat Cat: 39090 . COSPAR: 2013-009E. Apogee: 783 km (486 mi). Perigee: 771 km (479 mi). Inclination: 98.63 deg. Period: 100.40 min. 3U cubesat, a technical test project of Surrey Satellite and the Surrey Space Centre. Carried a Google Nexus One smartphone as its main avionics, and featured plasma thrusters and a water-alcohol thruster. Successful; first in STRaND Program..

• TUGSAT-1 - . Payload: BRITE-A. Mass: 10 kg (22 lb). Nation: Austria. Class: Astronomy. Type: Astronomy satellite. Spacecraft: Toronto GNB. USAF Sat Cat: 39091 . COSPAR: 2013-009F. Apogee: 784 km (487 mi). Perigee: 770 km (470 mi). Inclination: 98.63 deg. Period: 100.38 min. Satellite based on the Toronto Generic Nanosatellite Bus, built by the Technical University of Graz, Austra with help from UTIAS. Carried an 0.03m telescope-photometer for stellar photometry and astroseismology..

• UniBRITE - . Payload: BRITE-U. Mass: 10 kg (22 lb). Nation: Austria. Class: Astronomy. Type: Astronomy satellite. Spacecraft: Toronto GNB. USAF Sat Cat: 39092 . COSPAR: 2013-009G. Apogee: 783 km (486 mi). Perigee: 771 km (479 mi). Inclination: 98.63 deg. Period: 100.39 min. Nanosatellite built by UTIAS for the University of Vienna, Austria. Carried an 0.03m telescope-photometer for stellar photometry and astroseismology..

• IRNSS-1A - . Mass: 1,425 kg (3,141 lb). Nation: India. Class: Navigation. Type: Navigation satellite. Spacecraft: I-1K. USAF Sat Cat: 39199 . COSPAR: 2013-034A. Apogee: 35,866 km (22,286 mi). Perigee: 35,706 km (22,186 mi). Inclination: 27.35 deg. Period: 1,436.06 min. First Indian operational navigation satellite, beginning the Indian Regional Navigation Satellite System. Provides L-band and S-band navigation signals..

• Mars Orbiter Spacecraft - . Mass: 1,350 kg (2,970 lb). Nation: India. Class: Mars. Type: Mars probe. Spacecraft: Chandrayaan. USAF Sat Cat: 39370 . COSPAR: 2013-060A.

  First Indian mission to Mars. Carried 15 kg of instruments, including a color camera, but primary purpose was to test technologies for future planetary missions. Carried 850 kg of propellant for trans-Mars ejection and insertion into Martian orbit on arrival there. The MOS was inserted in elliptical Earth orbit; it used its own propulsion to achieve trans-Mars injection. The fourth stage and MOM payload entered a 251 x 23,892 km x 19.4 deg orbit with first perigee over the South Pacific. On November 7 the orbit was raised to 259 x 28,726 km, and on November 8 to over 70,000 km apogee. A further burn on November 10 delivered only 35 m/s, raising the apogee less than planned. A makeup burn on November 11 fixed the problem, and a burn on November 15 put the spacecraft in a 853 x 194,683 km x 19.4 deg orbit. A final perigee burn at 19:19 GMT on November 30 accelerated MOM to a hyperbolic Earth escape trajectory, and it entered an 0.98 x 1.45 AU solar orbit on December 3 on the way to Mars.

• Spot 7 - . Payload: AstroSat-500 Mk.2 (AstroBus-L). Mass: 712 kg (1,569 lb). Nation: France. Spacecraft: Astrobus. USAF Sat Cat: 40053 . COSPAR: 2014-034A. Apogee: 699 km (434 mi). Perigee: 697 km (433 mi). Inclination: 98.20 deg. Period: 98.73 min. Earth observation satellite with a 2 meter resolution on a 60 kilometer swath..

• Aisat - . Mass: 14 kg (30 lb). Nation: Germany. Spacecraft: Aisat. USAF Sat Cat: 40054 . COSPAR: 2014-034B. Apogee: 663 km (411 mi). Perigee: 639 km (397 mi). Inclination: 98.25 deg. Period: 97.75 min. DLR satellite with experimental Automatic Identification System (AIS) for tracking ships..

• NLS 7.1/Canx 4 - . Mass: 15 kg (33 lb). Nation: Canada. Spacecraft: Toronto GNB. USAF Sat Cat: 40055 . COSPAR: 2014-034C. Apogee: 661 km (410 mi). Perigee: 639 km (397 mi). Inclination: 98.25 deg. Period: 97.73 min. Univeristy of Toronto demonstration of on-orbit formation flying using differential GPS..

• NLS 7.2/Canx 5 - . Mass: 15 kg (33 lb). Nation: Canada. Spacecraft: Toronto GNB. USAF Sat Cat: 40056 . COSPAR: 2014-034D. Apogee: 662 km (411 mi). Perigee: 639 km (397 mi). Inclination: 98.25 deg. Period: 97.73 min.

• Velox 1 - . Mass: 4.00 kg (8.80 lb). Nation: Singapore. Spacecraft: Cubesat. USAF Sat Cat: 40057 . COSPAR: 2014-034E. Apogee: 658 km (408 mi). Perigee: 639 km (397 mi). Inclination: 98.25 deg. Period: 97.69 min. 3u cubesat by Singapore National Technical University; to have deployed the Velox P3 subsatellite..

• TeLEOS-1 - . Nation: USA. Class: Surveillance. Type: Surveillance satellite. COSPAR: 2015-077A. For AgilSpace, the 400 kg TeLEOS-1 satellite with a 1 meter resolution Earth imager. The satellite was built by Singapore Technologies Electronics, of which AgilSpace was a subsidiary..

• VELOX-C1 - . Mass: 123 kg (271 lb). Nation: USA. Class: Earth. Type: Weather satellite. COSPAR: 2015-077B. For Nanyang Technological University, the 123 kg VELOX-C1 carrying a GPS radio occultation payload for meteorology.

• Kent Ridge 1 - . Nation: USA. Class: Surveillance. Type: Surveillance satellite. COSPAR: 2015-077C.

  For the National University of Singapore, the 78 kg Kent Ridge 1 satellite developed using the TUBSAT LEOS-50 bus by Berlin Space Technologies, a spinoff of the old TUBSAT group at Technische Universitat Berlin. KR-1 carried two low-resoluton hyperspectral Earth imagers and a 6-meter-resolution imager.

• VELOX-II - . Nation: USA. Class: Technology. Type: Technology satellite. Spacecraft: Cubesat. COSPAR: 2015-077D. The 12 kg VELOX-II carried a space communications relay experiment to demonstrate cubesat downlink via geostationary communications satellite. VELOX-II was a 6U cubesat - only the 4th to be launched worldwide in this new larger cubesat format..

• Galassia - . Nation: USA. Class: Science. Type: Science satellite. Spacecraft: Cubesat. COSPAR: 2015-077E. A second NUS satellite was Galassia, a 2U cubesat with science payloads to measure the ionosphere and perform a quantum entanglement experiment..

• Athenoxat-1 - . Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. COSPAR: 2015-077F. In a technology development test, the PSLV 4th stage was reignited briefly to test its ability to deliver payloads to multiple orbits. For Microsat Rapid Pte Ltd., the 3U cubesat Athenoxat-1 carried a payload to image the night side of the Earth..

• IRNSS-1G - . Mass: 1,425 kg (3,141 lb). Nation: USA. Class: Navigation. Type: Navigation satellite. Spacecraft: I-1K. USAF Sat Cat: 41469 . COSPAR: 2016-027A. Apogee: 35,821 km (22,258 mi). Perigee: 35,741 km (22,208 mi). Inclination: 5.10 deg. Launch of the IRNSS-1G completed India's 7-satellite navigation constellation. Placed in geosynchronous orbit at 129 deg E..

• ScatSat-1 - . Nation: USA. Class: Earth. Type: Climate satellite. USAF Sat Cat: 41790 . COSPAR: 2016-059H. Apogee: 733 km (455 mi). Perigee: 717 km (445 mi). Inclination: 98.10 deg. 0915LT SSO ISRO ocean wind speed scatterometer mission..

• Pratham - . Nation: USA. Class: Technology. Type: Technology satellite. USAF Sat Cat: 41783 . COSPAR: 2016-059A. Apogee: 707 km (439 mi). Perigee: 660 km (410 mi). Inclination: 98.20 deg.

  India's PSLV-C35 vehicle was launched on Sep 26 with a cluster of small satellites. For the first time, the PS4 final stage made multiple burns to deliver payloads to different orbits. Its first burn reached a 718 x 732 km orbit at 0358 UTC, and ISRO's SCATSAT ocean wind speed scatterometer mission was deployed at 0359. At 0504 and 0554 UTC two more burns reached a 661 x 704 km orbit and the DLA dual launch adapter was ejected, followed by deployment of the remaining payloads. PRATHAM from IIT Bombay, with an ionospheric science instrument 0930LT SSO

• PISAT - . Nation: USA. Class: Technology. Type: Technology satellite. Spacecraft: Cubesat. USAF Sat Cat: 41784 . COSPAR: 2016-059B. Apogee: 705 km (438 mi). Perigee: 661 km (410 mi). Inclination: 98.20 deg. From PES University, Bangalore, with an 80m resolution imager 0930LT SSO.

• Pathfinder 1 - . Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 41787 . COSPAR: 2016-059E. Apogee: 703 km (436 mi). Perigee: 660 km (410 mi). Inclination: 98.20 deg. From Black Sky Global (Seattle) with a 1 meter imager 0930LT SSO.

• CanX-7 - . Nation: USA. Class: Technology. Type: Technology satellite. Spacecraft: Cubesat. USAF Sat Cat: 41788 . COSPAR: 2016-059F. Apogee: 702 km (436 mi). Perigee: 660 km (410 mi). Inclination: 98.20 deg. From UTIAS/Toronto, with a deployable deorbit sail 0930LT SSO.

• ALSAT-1B - . Nation: USA. Class: Surveillance. Type: Surveillance satellite. USAF Sat Cat: 41785 . COSPAR: 2016-059C. Apogee: 704 km (437 mi). Perigee: 661 km (410 mi). Inclination: 98.20 deg. 0930LT SSO imaging satellites for the Algerian space agency ASAL: ALSAT-1B built by Surrey.

• ALSAT-2B - . Nation: USA. Class: Surveillance. Type: Surveillance satellite. USAF Sat Cat: 41786 . COSPAR: 2016-059D. Apogee: 673 km (418 mi). Perigee: 672 km (417 mi). Inclination: 98.20 deg. 0930LT SSO built by Airbus/Toulouse.

• ALSAT-Nano - . Nation: USA. Class: Technology. Type: Technology satellite. Spacecraft: Cubesat. USAF Sat Cat: 41789 . COSPAR: 2016-059G. Apogee: 700 km (430 mi). Perigee: 660 km (410 mi). Inclination: 98.20 deg. 0930LT SSO cubesat built by Algerian engineers in Surrey and integrated in Algeria..

• Resourcesat-2A - . Nation: India. Class: Surveillance. Type: Surveillance satellite. USAF Sat Cat: 41877 . COSPAR: 2016-074A. Apogee: 831 km (516 mi). Perigee: 814 km (505 mi). Inclination: 98.70 deg. 1030LT SSO imaging satellite to provide continuity of service for the system as 2011's Resourcesat-2 ages. The satellite has a 6 metre resolution imager..

• Cartosat-2 Series/4 - . Payload: Cartosat 2D. Nation: India. Class: Surveillance. Type: Surveillance satellite. USAF Sat Cat: 41948 . COSPAR: 2017-008A. Apogee: 520 km (320 mi). Perigee: 505 km (313 mi). Inclination: 97.50 deg.

  See Cartosat 2D. India's PSLV placed a record 104 payloads in orbit on Feb 15, 100 of them via 25 QuadPack cubesat dispensers from the Dutch company ISISSpace. The main payload was the 714 kg `Cartosat-2 series satellite', the fourth such imaging payload from ISRO.

• INS-1A - . Nation: India. Class: Technology. Type: Technology satellite. USAF Sat Cat: 41949 . COSPAR: 2017-008B. Apogee: 508 km (315 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See INS 1A. 10 kg INS-1 (Indian Nanosatellite) technology payload..

• INS-1B - . Nation: India. Class: Surveillance. Type: Surveillance satellite. USAF Sat Cat: 41954 . COSPAR: 2017-008G. Apogee: 507 km (315 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See INS 1B. Two 10 kg INS-1 (Indian Nanosatellite) technology payloads..

• Al-Farabi 1 - . Nation: Kazakhstan. Class: Technology. Type: Technology satellite. Spacecraft: Cubesat. USAF Sat Cat: 42016 . COSPAR: 2017-008BW. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Al-Farabi 1. Cubesat for Al-Farabi Kazakh National University..

• PEASSS - . Nation: Netherlands. Class: Technology. Type: Technology satellite. Spacecraft: Cubesat. USAF Sat Cat: 42015 . COSPAR: 2017-008BV. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See PEASSS. Cubesat for Dutch research lab TNO..

• BGUSat - . Nation: Israel. Class: Technology. Type: Technology satellite. Spacecraft: Cubesat. USAF Sat Cat: 41999 . COSPAR: 2017-008BD. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See BGUSat. Cubesat for SpacePharma (a Swiss/Israeli company), Ben Gurion University..

• Dido-2 - . Nation: Israel. Class: Materials. Type: Materials science satellite. USAF Sat Cat: 42000 . COSPAR: 2017-008BE. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See DIDO 2 (Chen Jiayong 1). ..

• Nayif-1 - . Nation: UAE. Class: Technology. Type: Technology satellite. Spacecraft: Cubesat. USAF Sat Cat: 42017 . COSPAR: 2017-008BX. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Nayif 1 (FUNcube 5, EO 88, OSCAR 88). Cubesat for Rashid Space Center (Dubai)..

• Lemur-2-Satchmo - . Nation: USA. Class: Communications. Type: Communications satellite. Spacecraft: Cubesat. USAF Sat Cat: 41991 . COSPAR: 2017-008AV. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Lemur-2 24 (Lemur-2 Satchmo). ..

• Lemur-2-Mia-Grace - . Nation: USA. Class: Communications. Type: Communications satellite. Spacecraft: Cubesat. USAF Sat Cat: 41992 . COSPAR: 2017-008AW. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Lemur-2 27 (Lemur-2 Mia-Grace). ..

• Lemur-2-Smita-Sharad - . Nation: USA. Class: Communications. Type: Communications satellite. Spacecraft: Cubesat. USAF Sat Cat: 41993 . COSPAR: 2017-008AX. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Lemur-2 26 (Lemur-2 Smita-Sharad). ..

• Lemur-2-Spire-Minion - . Nation: USA. Class: Communications. Type: Communications satellite. Spacecraft: Cubesat. USAF Sat Cat: 41994 . COSPAR: 2017-008AY. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Lemur-2 23 (Lemur-2 Spire-Minions). ..

• Lemur-2-Rdeaton - . Nation: USA. Class: Communications. Type: Communications satellite. Spacecraft: Cubesat. USAF Sat Cat: 41995 . COSPAR: 2017-008AZ. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Lemur-2 25 (Lemur-2 Rdeaton). ..

• Lemur-2-NoguesCorrei - . Nation: USA. Class: Communications. Type: Communications satellite. Spacecraft: Cubesat. USAF Sat Cat: 41996 . COSPAR: 2017-008BA. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Lemur-2 28 (Lemur-2 NoguesCorreig). ..

• Lemur-2-Jopanbutra - . Nation: USA. Class: Communications. Type: Communications satellite. Spacecraft: Cubesat. USAF Sat Cat: 41997 . COSPAR: 2017-008BB. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Lemur-2 22 (Lemur-2 Jobanputra). ..

• Lemur-2-Tachikoma - . Nation: USA. Class: Communications. Type: Communications satellite. Spacecraft: Cubesat. USAF Sat Cat: 41998 . COSPAR: 2017-008BC. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Lemur-2 29 (Lemur-2 Tachikoma). ..

• Flock 3p-1 - . Payload: Dove 1000. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 41967 . COSPAR: 2017-008V. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 1 (Dove 1000). ..

• Flock 3p-2 - . Payload: Dove 1001. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 41966 . COSPAR: 2017-008U. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 2 (Dove 1001). ..

• Flock 3p-3 - . Payload: Dove 1002. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 41968 . COSPAR: 2017-008W. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 3 (Dove 1002). ..

• Flock 3p-4 - . Payload: Dove 1003. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 41965 . COSPAR: 2017-008T. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 4 (Dove 1003). ..

• Flock 3p-5 - . Payload: Dove 0F18. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 41971 . COSPAR: 2017-008Z. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 5 (Dove 0F18). ..

• Flock 3p-6 - . Payload: Dove 0F35. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 41969 . COSPAR: 2017-008X. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 6 (Dove 0F35). ..

• Flock 3p-7 - . Payload: Dove 100B. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 41970 . COSPAR: 2017-008Y. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 7 (Dove 100B). ..

• Flock 3p-8 - . Payload: Dove 100C. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 41951 . COSPAR: 2017-008D. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 8 (Dove 100C). ..

• Flock 3p-9 - . Payload: Dove 1021. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 41973 . COSPAR: 2017-008AB. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 9 (Dove 1021). ..

• Flock 3p-10 - . Payload: Dove 1022. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 41974 . COSPAR: 2017-008AC. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 10 (Dove 1022). ..

• Flock 3p-11 - . Payload: Dove 101F. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 41975 . COSPAR: 2017-008AD. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 11 (Dove 101F). ..

• Flock 3p-12 - . Payload: Dove 1010. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 41972 . COSPAR: 2017-008AA. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 12 (Dove 1010). ..

• Flock 3p-13 - . Payload: Dove 1016. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 42040 . COSPAR: 2017-008CW. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 13 (Dove 1016). ..

• Flock 3p-14 - . Payload: Dove 1018. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 42012 . COSPAR: 2017-008BS. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 14 (Dove 1018). ..

• Flock 3p-15 - . Payload: Dove 101D. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 42039 . COSPAR: 2017-008CV. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 15 (Dove 101D). ..

• Flock 3p-16 - . Payload: Dove 100E. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 42011 . COSPAR: 2017-008BR. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 16 (Dove 100E). ..

• Flock 3p-17 - . Payload: Dove 1023. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 41962 . COSPAR: 2017-008Q. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 17 (Dove 1023). ..

• Flock 3p-18 - . Payload: Dove 102B. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 41957 . COSPAR: 2017-008K. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 18 (Dove 102B). ..

• Flock 3p-19 - . Payload: Dove 1024. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 41955 . COSPAR: 2017-008H. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 19 (Dove 1024). ..

• Flock 3p-20 - . Payload: Dove 1029. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 41950 . COSPAR: 2017-008C. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 20 (Dove 1029). ..

• Flock 3p-21 - . Payload: Dove 102A. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 41959 . COSPAR: 2017-008M. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 21 (Dove 102A). ..

• Flock 3p-22 - . Payload: Dove 1028. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 41958 . COSPAR: 2017-008L. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 22 (Dove 1028). ..

• Flock 3p-23 - . Payload: Dove 1025. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 42018 . COSPAR: 2017-008BY. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 23 (Dove 1025). ..

• Flock 3p-24 - . Payload: Dove 1026. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 41956 . COSPAR: 2017-008J. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 24 (Dove 1026). ..

• Flock 3p-25 - . Payload: Dove 102F. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 41964 . COSPAR: 2017-008S. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 25 (Dove 102F). ..

• Flock 3p-26 - . Payload: Dove 102D. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 41961 . COSPAR: 2017-008P. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 26 (Dove 102D). ..

• Flock 3p-27 - . Payload: Dove 1030. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 41963 . COSPAR: 2017-008R. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 27 (Dove 1030). ..

• Flock 3p-28 - . Payload: Dove 102C. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 41960 . COSPAR: 2017-008N. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 28 (Dove 102C). ..

• Flock 3p-29 - . Payload: Dove 1033. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 42045 . COSPAR: 2017-008DB. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 29 (Dove 1033). ..

• Flock 3p-30 - . Payload: Dove 102E. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 41987 . COSPAR: 2017-008AR. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 30 (Dove 102E). ..

• Flock 3p-31 - . Payload: Dove 1032. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 42049 . COSPAR: 2017-008DF. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 31 (Dove 1032). ..

• Flock 3p-32 - . Payload: Dove 1035. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 42023 . COSPAR: 2017-008CD. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 32 (Dove 1035). ..

• Flock 3p-33 - . Payload: Dove 103C. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 41990 . COSPAR: 2017-008AU. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 33 (Dove 103C). ..

• Flock 3p-34 - . Payload: Dove 103B. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 41988 . COSPAR: 2017-008AS. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 34 (Dove 103B). ..

• Flock 3p-35 - . Payload: Dove 103D. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 41989 . COSPAR: 2017-008AT. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 35 (Dove 103D). ..

• Flock 3p-36 - . Payload: Dove 103A. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 41986 . COSPAR: 2017-008AQ. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 36 (Dove 103A). ..

• Flock 3p-37 - . Payload: Dove 1037. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 41953 . COSPAR: 2017-008F. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 37 (Dove 1037). ..

• Flock 3p-38 - . Payload: Dove 1036. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 42037 . COSPAR: 2017-008CT. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 38 (Dove 1036). ..

• Flock 3p-39 - . Payload: Dove 103E. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 42038 . COSPAR: 2017-008CU. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 39 (Dove 103E). ..

• Flock 3p-40 - . Payload: Dove 1039. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 42010 . COSPAR: 2017-008BQ. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 40 (Dove 1039). ..

• Flock 3p-41 - . Payload: Dove 1031. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 42004 . COSPAR: 2017-008BJ. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 41 (Dove 1031). ..

• Flock 3p-42 - . Payload: Dove 101E. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 42008 . COSPAR: 2017-008BN. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 42 (Dove 101E). ..

• Flock 3p-43 - . Payload: Dove 1041. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 42007 . COSPAR: 2017-008BM. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 43 (Dove 1041). ..

• Flock 3p-44 - . Payload: Dove 1019. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 42033 . COSPAR: 2017-008CP. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 44 (Dove 1019). ..

• Flock 3p-45 - . Payload: Dove 101A. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 42005 . COSPAR: 2017-008BK. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 45 (Dove 101A). ..

• Flock 3p-46 - . Payload: Dove 1011. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 42031 . COSPAR: 2017-008CM. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 46 (Dove 1011). ..

• Flock 3p-47 - . Payload: Dove 1027. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 42032 . COSPAR: 2017-008CN. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 47 (Dove 1027). ..

• Flock 3p-48 - . Payload: Dove 1042. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 42006 . COSPAR: 2017-008BL. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 48 (Dove 1042). ..

• Flock 3p-49 - . Payload: Dove 1038. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 42001 . COSPAR: 2017-008BF. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 49 (Dove 1038). ..

• Flock 3p-50 - . Payload: Dove 1034. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 42029 . COSPAR: 2017-008CK. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 50 (Dove 1034). ..

• Flock 3p-51 - . Payload: Dove 1006. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 41952 . COSPAR: 2017-008E. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 51 (Dove 1006). ..

• Flock 3p-52 - . Payload: Dove 1044. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 42030 . COSPAR: 2017-008CL. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 52 (Dove 1044). ..

• Flock 3p-53 - . Payload: Dove 1007. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 42013 . COSPAR: 2017-008BT. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 53 (Dove 1007). ..

• Flock 3p-54 - . Payload: Dove 1005. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 42014 . COSPAR: 2017-008BU. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 54 (Dove 1005). ..

• Flock 3p-55 - . Payload: Dove 1008. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 42041 . COSPAR: 2017-008CX. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 55 (Dove 1008). ..

• Flock 3p-56 - . Payload: Dove 100F. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 42042 . COSPAR: 2017-008CY. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 56 (Dove 100F). ..

• Flock 3p-57 - . Payload: Dove 1014. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 41978 . COSPAR: 2017-008AG. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 57 (Dove 1014). ..

• Flock 3p-58 - . Payload: Dove 1009. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 41977 . COSPAR: 2017-008AF. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 58 (Dove 1009). ..

• Flock 3p-59 - . Payload: Dove 1045. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 42021 . COSPAR: 2017-008CB. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 59 (Dove 1045). ..

• Flock 3p-60 - . Payload: Dove 101B. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 41976 . COSPAR: 2017-008AE. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 60 (Dove 101B). ..

• Flock 3p-61 - . Payload: Dove 1012. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 42009 . COSPAR: 2017-008BP. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 61 (Dove 1012). ..

• Flock 3p-62 - . Payload: Dove 1046. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 42036 . COSPAR: 2017-008CS. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 62 (Dove 1046). ..

• Flock 3p-63 - . Payload: Dove 1015. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 42035 . COSPAR: 2017-008CR. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 63 (Dove 1015). ..

• Flock 3p-64 - . Payload: Dove 100A. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 42034 . COSPAR: 2017-008CQ. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 64 (Dove 100A). ..

• Flock 3p-65 - . Payload: Dove 1040. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 42028 . COSPAR: 2017-008CJ. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 65 (Dove 1040). ..

• Flock 3p-66 - . Payload: Dove 1013. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 42027 . COSPAR: 2017-008CH. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 66 (Dove 1013). ..

• Flock 3p-67 - . Payload: Dove 1017. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 42002 . COSPAR: 2017-008BG. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 67 (Dove 1017). ..

• Flock 3p-68 - . Payload: Dove 1004. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 42003 . COSPAR: 2017-008BH. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 68 (Dove 1004). ..

• Flock 3p-69 - . Payload: Dove 0F43. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 42019 . COSPAR: 2017-008BZ. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 69 (Dove 0F43). ..

• Flock 3p-70 - . Payload: Dove 0F15. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 41980 . COSPAR: 2017-008AJ. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 70 (Dove 0F15). ..

• Flock 3p-71 - . Payload: Dove 0F11. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 42051 . COSPAR: 2017-008DH. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 71 (Dove 0F11). ..

• Flock 3p-72 - . Payload: Dove 0F10. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 42024 . COSPAR: 2017-008CE. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 72 (Dove 0F10). ..

• Flock 3p-73 - . Payload: Dove 0F1B. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 41981 . COSPAR: 2017-008AK. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 73 (Dove 0F1B). ..

• Flock 3p-74 - . Payload: Dove 0F22. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 42048 . COSPAR: 2017-008DE. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 74 (Dove 0F22). ..

• Flock 3p-75 - . Payload: Dove 0F12. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 41979 . COSPAR: 2017-008AH. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 75 (Dove 0F12). ..

• Flock 3p-76 - . Payload: Dove 0F17. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 42020 . COSPAR: 2017-008CA. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 76 (Dove 0F17). ..

• Flock 3p-77 - . Payload: Dove 0F28. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 42025 . COSPAR: 2017-008CF. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 77 (Dove 0F28). ..

• Flock 3p-78 - . Payload: Dove 0F51. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 42047 . COSPAR: 2017-008DD. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 78 (Dove 0F51). ..

• Flock 3p-79 - . Payload: Dove 0F52. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 41984 . COSPAR: 2017-008AN. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 79 (Dove 0F52). ..

• Flock 3p-80 - . Payload: Dove 0F4E. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 42026 . COSPAR: 2017-008CG. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 80 (Dove 0F4E). ..

• Flock 3p-81 - . Payload: Dove 0F25. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 42043 . COSPAR: 2017-008CZ. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 81 (Dove 0F25). ..

• Flock 3p-82 - . Payload: Dove 0F41. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 42046 . COSPAR: 2017-008DC. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 82 (Dove 0F41). ..

• Flock 3p-83 - . Payload: Dove 0F3F. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 42050 . COSPAR: 2017-008DG. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 83 (Dove 0F3F). ..

• Flock 3p-84 - . Payload: Dove 0F42. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 42022 . COSPAR: 2017-008CC. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 84 (Dove 0F42). ..

• Flock 3p-85 - . Payload: Dove 0F1D. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 41983 . COSPAR: 2017-008AM. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 85 (Dove 0F1D). ..

• Flock 3p-86 - . Payload: Dove 0F34. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 41985 . COSPAR: 2017-008AP. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 86 (Dove 0F34). ..

• Flock 3p-87 - . Payload: Dove 0F31. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 42044 . COSPAR: 2017-008DA. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 87 (Dove 0F31). ..

• Flock 3p-88 - . Payload: Dove 0F38. Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft: Cubesat. USAF Sat Cat: 41982 . COSPAR: 2017-008AL. Apogee: 506 km (314 mi). Perigee: 496 km (308 mi). Inclination: 97.50 deg. See Flock-3p 88 (Dove 0F38). ..