El Arenosillo
Credit: © Mark Wade
Spain
More... - Chronology...
Associated People
-
Disney Disney, Walt (1901-1966) Spanish-American creator of children's movies and amusement parks; produced a series of three crucial television programs in 1955-1957 that popularized von Braun's concepts for manned orbital, lunar, and Mars travel with the American public. More...
-
Sponable Sponable, Jess Mitchell (1955-) American engineer military spaceflight engineer astronaut, 1982-1987. More...
-
Lopez-Alegria Lopez-Alegria, Michael Eladio 'LA' (1958-) Spanish-American test pilot mission specialist astronaut. Flew on STS-73, STS-92, STS-113, ISS EO-14. More...
-
Duque Duque, Pedro Francisco (1963-) Spanish engineer mission specialist astronaut. Flew on STS-95, ISS Cervantes. First Spanish astronaut. More...
Associated Spacecraft
-
Escafandra Estratonautica Spanish pressure suit. Spanish Colonel Don Emilio Herrera Linares designed and built a full pressure suit in 1935, which was to have been used during an open-basket balloon stratospheric flight scheduled for early 1936. More...
-
Intasat Spanish communications technology satellite. One launch, 1974.11.15. Spanish communications satellite. More...
-
LBSAT Spanish communications technology satellite. One launch, 1995.07.07, UPM/LBSAT 1. Universidad Politecnia de Madrid Satellite; experimental communications, microgravity experiments. More...
-
Nanosat 01 Spanish technology satellite. One launch, 2004.12.18. Experimental nanosat built by the Spanish space agency (INTA). More...
Associated Launch Vehicles
-
INTA The Instituto Nacional de Tecnica Aerospacial was tasked in 1967 to develop Spain's first sounding rocket. INTA contracted with British Aerojet to provide the necessary technical expertise and designed a rocket built from existing British solid motors. This was followed by versions using Spanish-manufactured versions of British motors. The stop-and-go program extended over nearly 30 years. More...
-
INTA-255 Spanish sounding rocket. Vehicle consisting of 4 x Chick + 1 x Goose. All motors ignited simultaneously at lift-off, the Chicks burning for 0.2 seconds, while the Goose continued for 17 seconds. More...
-
INTA-300 Spanish sounding rocket. Two stage vehicle consisting of 1 x Heron + 1 x Snipe More...
-
INTA-300B Spanish sounding rocket. Later version for heavier payloads fired in 1993-1994. More...
-
Capricorno Spanish all-solid orbital launch vehicle. Small all-solid-propellant launch vehicle pursued by Spain in 1992-1999. Cancelled in 2000 before any flights could be made. More...
Associated Manufacturers and Agencies
-
INTA Spanish agency overseeing development of rockets and spacecraft. Instituto Nacional de Tecnica Aeroespacial, Torrejon, Spain. More...
-
UPM Spanish manufacturer of spacecraft. Madrid Polytechnic University, Madrid, Spain. More...
-
CASA Spanish manufacturer of spacecraft. Construcciones Aeronauticas SA, Madrid, Spain. More...
Associated Programs
Associated Launch Sites
-
El Arenosillo Spanish sounding rocket launch location known to have been used for 335 launches from 1966 to 1994, reaching up to 700 kilometers altitude. More...
-
Gando Launch site on Canary Islands, near NASA tracking station, considered for several planned Spanish and Italian orbital launch vehicles. L-1011 carrier aircraft staging from Gran Canaria air-launch Pegasus launch vehicles into orbit near here (drop point 27.00 N 15.30 W). More...
Associated Stages
Spain Chronology
1955 November 29 - .
1958 May 30 - .
1963 March 14 - .
- Birth of Pedro Francisco Duque - .
Nation: Spain. Summary: Spanish engineer mission specialist astronaut. Flew on STS-95, ISS Cervantes. First Spanish astronaut..
1966 October 15 - .
Launch Site:
El Arenosillo.
LV Family:
Skua.
Launch Vehicle:
Skua 1.
- Carabela 4 Aeronomy / test - .
Nation: Spain. Agency: INTA. Apogee: 81 km (50 mi).
1966 October 20 - .
Launch Site:
El Arenosillo.
LV Family:
Skua.
Launch Vehicle:
Skua 1.
FAILURE: Failure.
- Aeronomy / test - .
Nation: Spain. Agency: INTA. Apogee: 0 km ( mi).
1966 Nov - .
Launch Site:
El Arenosillo.
Launch Vehicle:
Judi-Dart.
LV Configuration: Judi-Dart INTA Met.
- - .
Nation: Spain. Agency: INTA. Apogee: 70 km (43 mi).
1966 Nov - .
Launch Site:
El Arenosillo.
Launch Vehicle:
Skua.
- - .
Nation: Spain. Agency: INTA. Apogee: 75 km (46 mi).
1966 Nov - .
Launch Site:
El Arenosillo.
Launch Vehicle:
Skua.
- - .
Nation: Spain. Agency: INTA. Apogee: 75 km (46 mi).
1969 July 19 - .
Launch Site:
El Arenosillo.
LV Family:
INTA.
Launch Vehicle:
INTA-255.
LV Configuration: INTA-255 1.
- Booster test - .
Nation: Spain. Agency: INTA. Apogee: 1.00 km (0.60 mi).
1969 December 20 - .
Launch Site:
El Arenosillo.
LV Family:
INTA.
Launch Vehicle:
INTA-255.
LV Configuration: INTA-255 2.
- Test mission - .
Nation: Spain. Agency: INTA. Apogee: 73 km (45 mi).
1970 December 22 - .
Launch Site:
El Arenosillo.
LV Family:
INTA.
Launch Vehicle:
INTA-255.
LV Configuration: INTA-255 3.
- Test mission - .
Nation: Spain. Agency: INTA. Apogee: 132 km (82 mi).
1971 May 21 - .
22:35 GMT - .
Launch Site:
El Arenosillo.
LV Family:
Skua.
Launch Vehicle:
Skua 2.
LV Configuration: Skua 2 INTA SA-7101.
- Ionosphere mission - .
Nation: Spain. Agency: INTA. Apogee: 81 km (50 mi).
1971 May 26 - .
23:31 GMT - .
Launch Site:
El Arenosillo.
LV Family:
Cajun.
Launch Vehicle:
Nike Cajun.
LV Configuration: Nike Cajun INTA NC-7102.
- Ionosphere mission - .
Nation: Spain. Agency: INTA. Apogee: 145 km (90 mi).
1971 May 27 - .
01:41 GMT - .
Launch Site:
El Arenosillo.
LV Family:
Cajun.
Launch Vehicle:
Nike Cajun.
LV Configuration: Nike Cajun INTA NC-7103.
- Ionosphere mission - .
Nation: Spain. Agency: INTA. Apogee: 152 km (94 mi).
1971 May 28 - .
02:52 GMT - .
Launch Site:
El Arenosillo.
LV Family:
Cajun.
Launch Vehicle:
Nike Cajun.
LV Configuration: Nike Cajun INTA NC-7104.
- Ionosphere mission - .
Nation: Spain. Agency: INTA. Apogee: 160 km (90 mi).
1971 May 28 - .
04:31 GMT - .
Launch Site:
El Arenosillo.
LV Family:
Skua.
Launch Vehicle:
Skua 2.
LV Configuration: Skua 2 INTA SC-7102.
- Ionosphere mission - .
Nation: Spain. Agency: INTA. Apogee: 103 km (64 mi).
1974 November 15 - .
17:11 GMT - .
Launch Site:
Vandenberg.
Launch Complex:
Vandenberg SLC2W.
LV Family:
Delta.
Launch Vehicle:
Delta 2310.
LV Configuration: Delta 2310 592/D104.
- Intasat 1 - .
Payload: Intasat. Mass: 20 kg (44 lb). Nation: Spain. Agency: INTA. Class: Technology. Type: Communications technology satellite. Spacecraft: Intasat. USAF Sat Cat: 7531 . COSPAR: 1974-089C. Apogee: 1,459 km (906 mi). Perigee: 1,442 km (896 mi). Inclination: 101.8000 deg. Period: 114.90 min.
1976 Jan - .
Launch Site:
El Arenosillo.
Launch Vehicle:
Super Loki.
- Winter Anomaly - .
Nation: Spain. Agency: INTA. Apogee: 70 km (43 mi).
1976 January 2 - .
14:59 GMT - .
Launch Site:
El Arenosillo.
LV Family:
Skua.
Launch Vehicle:
Skua 3.
LV Configuration: Skua 3 INTA S3CLO-76001.
- Aeronomy / ionosphere mission - .
Nation: Spain. Agency: INTA; DLR. Apogee: 94 km (58 mi).
1976 January 4 - .
13:40 GMT - .
Launch Site:
El Arenosillo.
LV Family:
Petrel.
Launch Vehicle:
Petrel 1.
LV Configuration: Petrel INTA MPGA-76001.
- Winter Anomaly Ionosphere mission - .
Nation: Spain. Agency: DLR; INTA. Apogee: 84 km (52 mi).
1976 January 4 - .
16:00 GMT - .
Launch Site:
El Arenosillo.
LV Family:
Petrel.
Launch Vehicle:
Petrel 1.
LV Configuration: Petrel INTA UCLP-76001.
- Winter Anomaly B-VI-1 Aeronomy mission - .
Nation: Spain. Agency: INTA. Apogee: 135 km (83 mi).
1976 January 20 - .
13:40 GMT - .
Launch Site:
El Arenosillo.
LV Family:
Petrel.
Launch Vehicle:
Petrel 1.
LV Configuration: Petrel INTA MPGA-76002.
- Winter Anomaly Ionosphere mission - .
Nation: Spain. Agency: DLR; INTA. Apogee: 60 km (37 mi).
1976 January 21 - .
13:40 GMT - .
Launch Site:
El Arenosillo.
LV Family:
Petrel.
Launch Vehicle:
Petrel 1.
LV Configuration: Petrel INTA MPGA-76003.
- Winter Anomaly Aeronomy / ionosphere mission - .
Nation: Spain. Agency: DLR; INTA. Apogee: 79 km (49 mi).
1976 January 21 - .
15:55 GMT - .
Launch Site:
El Arenosillo.
LV Family:
Petrel.
Launch Vehicle:
Petrel 1.
LV Configuration: Petrel INTA UCLP-76002.
- Winter Anomaly B-VI-2 Aeronomy mission - .
Nation: Spain. Agency: INTA; SRC. Apogee: 140 km (80 mi).
1976 January 21 - .
18:17 GMT - .
Launch Site:
El Arenosillo.
LV Family:
Petrel.
Launch Vehicle:
Petrel 1.
LV Configuration: Petrel INTA UCLP-76003.
- Winter Anomaly B-VI-3 Aeronomy mission - .
Nation: Spain. Agency: INTA; SRC. Apogee: 135 km (83 mi).
1976 February 8 - .
14:26 GMT - .
Launch Site:
El Arenosillo.
LV Family:
Petrel.
Launch Vehicle:
Petrel 1.
LV Configuration: Petrel INTA MPGA-76004.
- Aeronomy / ionosphere mission - .
Nation: Spain. Agency: DLR; INTA. Apogee: 81 km (50 mi).
1976 May 5 - .
Launch Site:
El Arenosillo.
LV Family:
Skua.
Launch Vehicle:
Skua 2.
LV Configuration: Skua 2 INTA MSCL-7608.
- Ionosphere mission - .
Nation: Spain. Agency: INTA; DLR. Apogee: 95 km (59 mi).
1978 June 28 - .
Launch Site:
El Arenosillo.
LV Family:
INTA.
Launch Vehicle:
INTA-300.
FAILURE: Failure.
- Aeronomy mission - .
Nation: Spain. Agency: INTA. Apogee: 0 km ( mi).
1981 February 18 - .
Launch Site:
El Arenosillo.
LV Family:
INTA.
Launch Vehicle:
INTA-300.
- Aeronomy mission - .
Nation: Spain. Agency: INTA. Apogee: 285 km (177 mi). Summary: First completely successful launch..
1981 December 19 - .
20:00 GMT - .
Launch Site:
El Arenosillo.
LV Family:
Petrel.
Launch Vehicle:
Petrel 1.
- FOCCA I Aeronomy mission - .
Nation: Spain. Agency: INTA. Apogee: 106 km (65 mi).
1982 March 13 - .
Launch Site:
El Arenosillo.
LV Family:
Petrel.
Launch Vehicle:
Petrel 1.
FAILURE: Failure.
- FOCCA II Aeronomy mission - .
Nation: Spain. Agency: INTA. Apogee: 140 km (80 mi).
1984 - .
Launch Site:
El Arenosillo.
Launch Vehicle:
INTA.
LV Configuration: INTA-100 3.
- Test - .
Nation: Spain. Agency: INTA. Apogee: 100 km (60 mi).
1984 - .
Launch Site:
El Arenosillo.
Launch Vehicle:
INTA.
LV Configuration: INTA-100 2.
- Test - .
Nation: Spain. Agency: INTA. Apogee: 100 km (60 mi).
1984 Jun - .
Launch Site:
El Arenosillo.
Launch Vehicle:
INTA.
LV Configuration: INTA-100 1.
- Test - .
Nation: Spain. Agency: INTA. Apogee: 100 km (60 mi).
1985 - .
Launch Site:
El Arenosillo.
Launch Vehicle:
INTA.
LV Configuration: INTA-100 4.
- Test - .
Nation: Spain. Agency: INTA. Apogee: 100 km (60 mi).
1985 - .
Launch Site:
El Arenosillo.
Launch Vehicle:
INTA.
LV Configuration: INTA-100 6.
- Test - .
Nation: Spain. Agency: INTA. Apogee: 100 km (60 mi).
1985 - .
Launch Site:
El Arenosillo.
Launch Vehicle:
INTA.
LV Configuration: INTA-100 5.
- Test - .
Nation: Spain. Agency: INTA. Apogee: 100 km (60 mi).
1990 - .
Launch Site:
El Arenosillo.
Launch Vehicle:
INTA.
LV Configuration: INTA-100 8.
- Test - .
Nation: Spain. Agency: INTA. Apogee: 100 km (60 mi).
1990 - .
Launch Site:
El Arenosillo.
Launch Vehicle:
INTA.
LV Configuration: INTA-100 7.
- Test - .
Nation: Spain. Agency: INTA. Apogee: 100 km (60 mi).
1990 - .
Launch Site:
El Arenosillo.
Launch Vehicle:
INTA.
LV Configuration: INTA-100 9.
- Test - .
Nation: Spain. Agency: INTA. Apogee: 100 km (60 mi).
1991 - .
Launch Site:
El Arenosillo.
Launch Vehicle:
INTA.
LV Configuration: INTA-100 11.
- Test - .
Nation: Spain. Agency: INTA. Apogee: 100 km (60 mi).
1991 - .
Launch Site:
El Arenosillo.
Launch Vehicle:
INTA.
LV Configuration: INTA-100 10.
- Test - .
Nation: Spain. Agency: INTA. Apogee: 100 km (60 mi).
1991 - .
Launch Site:
El Arenosillo.
Launch Vehicle:
INTA.
LV Configuration: INTA-100 12.
- Test - .
Nation: Spain. Agency: INTA. Apogee: 100 km (60 mi).
1992 September 10 - .
23:04 GMT - .
Launch Site:
Kourou.
Launch Complex:
Kourou ELA2.
LV Family:
Ariane.
Launch Vehicle:
Ariane 44LP.
LV Configuration: Ariane 44LP+ V53.
- Hispasat 1A - .
Mass: 2,194 kg (4,836 lb). Nation: Spain. Agency: Hispasat. Manufacturer: Toulouse. Program: Hispasat. Class: Communications. Type: Civilian communications satellite. Spacecraft: Eurostar 2000. USAF Sat Cat: 22116 . COSPAR: 1992-060A. Apogee: 35,794 km (22,241 mi). Perigee: 35,784 km (22,235 mi). Inclination: 0.1000 deg. Period: 1,436.20 min. Summary: Stationed at 30 deg W. Positioned in geosynchronous orbit at 30 deg W in 1992-1999 As of 3 September 2001 located at 29.99 deg W drifting at 0.013 deg W per day. As of 2007 Mar 10 located at 83.37E drifting at 3.458W degrees per day..
1993 July 22 - .
22:58 GMT - .
Launch Site:
Kourou.
Launch Complex:
Kourou ELA2.
LV Family:
Ariane.
Launch Vehicle:
Ariane 44L.
LV Configuration: Ariane 44L+ V58.
- Hispasat-1B - .
Mass: 2,120 kg (4,670 lb). Nation: Spain. Agency: Hispasat. Manufacturer: Toulouse. Program: Hispasat. Class: Communications. Type: Civilian communications satellite. Spacecraft: Eurostar 2000. USAF Sat Cat: 22723 . COSPAR: 1993-048A. Apogee: 35,794 km (22,241 mi). Perigee: 35,780 km (22,230 mi). Inclination: 0.0000 deg. Period: 1,436.10 min. Summary: Stationed at 30 deg W. Positioned in geosynchronous orbit at 30 deg W in 1993-1999 As of 5 September 2001 located at 30.13 deg W drifting at 0.024 deg W per day. As of 2007 Mar 8 located at 157.75E drifting at 1.953W degrees per day..
1993 October 21 - .
01:46 GMT - .
Launch Site:
El Arenosillo.
LV Family:
INTA.
Launch Vehicle:
INTA-300B.
LV Configuration: INTA-300B IAA.
- FEIROX / FEIROH Aeronomy mission - .
Nation: Spain. Agency: INTA. Apogee: 154 km (95 mi).
1994 April 16 - .
01:22 GMT - .
Launch Site:
El Arenosillo.
LV Family:
INTA.
Launch Vehicle:
INTA-300B.
LV Configuration: INTA-300B IAA.
- O2-INTA300 Aeronomy mission - .
Nation: Spain. Agency: INTA. Apogee: 156 km (96 mi).
1995 July 7 - .
16:23 GMT - .
Launch Site:
Kourou.
Launch Complex:
Kourou ELA2.
LV Family:
Ariane.
Launch Vehicle:
Ariane 40.
LV Configuration: Ariane 40 V75.
- UPM/LBSAT 1 - .
Mass: 47 kg (103 lb). Nation: Spain. Agency: UPM. Class: Technology. Type: Communications technology satellite. Spacecraft: LBSAT. USAF Sat Cat: 23607 . COSPAR: 1995-033C. Apogee: 676 km (420 mi). Perigee: 663 km (411 mi). Inclination: 98.1000 deg. Period: 98.10 min. Summary: Universidad Politecnia de Madrid Satellite; experimental communications, microgravity experiments..
2000 February 3 - .
23:30 GMT - .
Launch Site:
Cape Canaveral.
Launch Complex:
Cape Canaveral LC36B.
Launch Pad: SLC36B.
LV Family:
Atlas.
Launch Vehicle:
Atlas IIAS.
LV Configuration: Atlas IIAS AC-158.
- Hispasat 1C - .
Mass: 3,112 kg (6,860 lb). Nation: Spain. Agency: Hispasat. Manufacturer: Cannes. Program: Hispasat. Class: Communications. Type: Civilian communications satellite. Spacecraft: Spacebus 3000. USAF Sat Cat: 26071 . COSPAR: 2000-007A. Apogee: 35,796 km (22,242 mi). Perigee: 35,778 km (22,231 mi). Inclination: 0.0000 deg. Period: 1,436.10 min. Spanish domestic geosynchronous communications satellite. Stationed at 30 deg W. Positioned in geosynchronous orbit at 30 deg W in 2000. As of 3 September 2001 located at 30.14 deg W drifting at 0.013 deg W per day. As of 2007 Mar 9 located at 30.01W drifting at 0.005W degrees per day.
2002 September 18 - .
22:04 GMT - .
Launch Site:
Cape Canaveral.
Launch Complex:
Cape Canaveral LC36A.
Launch Pad: SLC36A.
LV Family:
Atlas.
Launch Vehicle:
Atlas IIAS.
LV Configuration: Atlas IIAS AC-159.
- Hispasat 1D - .
Mass: 3,250 kg (7,160 lb). Nation: Spain. Agency: Hispasat. Manufacturer: Cannes. Program: Hispasat. Class: Communications. Type: Civilian communications satellite. Spacecraft: Spacebus 3000. USAF Sat Cat: 27528 . COSPAR: 2002-044A. Apogee: 35,802 km (22,246 mi). Perigee: 35,772 km (22,227 mi). Inclination: 0.0000 deg. Period: 1,436.10 min. Launch delayed from May 28, August 14. Hispasat 1D was a Spanish geostationary communications spacecraft. The 3.3-ton, 7.0-kW satellite carried three antennae looking in different directions to provide video, data, and Internet services to Europe, North America, and North Africa via 28 Ku-band transponders after being parked over 30° W longitude alongside Hispasat 1A, 1B, and 1C. As of 2007 Mar 9 located at 29.97W drifting at 0.014W degrees per day.
2004 August 4 - .
22:32 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC200/39.
LV Family:
Proton.
Launch Vehicle:
Proton/Briz M.
LV Configuration: Proton-M/Briz-M 535-07.
- Amazonas - .
Payload: Eurostar 3000S. Mass: 4,545 kg (10,020 lb). Nation: Spain. Agency: Hispasat. Manufacturer: EADS Astrium. Program: Hispasat. Class: Communications. Type: Civilian communications satellite. Spacecraft: Spacebus 3000. USAF Sat Cat: 28393 . COSPAR: 2004-031A. Apogee: 35,791 km (22,239 mi). Perigee: 35,783 km (22,234 mi). Inclination: 0.1000 deg. Period: 1,436.10 min. Summary: Delayed from June, July 25. As of 2007 Mar 10 located at 61.03W drifting at 0.005W degrees per day..
2004 December 18 - .
16:26 GMT - .
Launch Site:
Kourou.
Launch Complex:
Kourou ELA3.
LV Family:
Ariane 5.
Launch Vehicle:
Ariane 5Gp.
LV Configuration: Ariane 5G+ V165.
- Nanosat 01 - .
Mass: 20 kg (44 lb). Nation: Spain. Agency: Arianespace. Manufacturer: INTA. Class: Technology. Type: Navigation technology satellite. Spacecraft: Nanosat 01. USAF Sat Cat: 28493 . COSPAR: 2004-049B. Apogee: 666 km (413 mi). Perigee: 658 km (408 mi). Inclination: 98.1000 deg. Period: 98.00 min. Summary: Experimental nanosat built by the Spanish space agency (INTA)..
2005 February 12 - .
21:03 GMT - .
Launch Site:
Kourou.
Launch Complex:
Kourou ELA3.
LV Family:
Ariane 5.
Launch Vehicle:
Ariane 5ECA.
LV Configuration: Ariane 5ECA V164 (521) City of Bremen.
- XTAR-EUR - .
Mass: 3,631 kg (8,004 lb). Nation: Spain. Agency: ESA. Manufacturer: Palo Alto. Class: Communications. Type: Civilian communications satellite. Spacecraft: FS-1300. USAF Sat Cat: 28542 . COSPAR: 2005-005A. Apogee: 35,794 km (22,241 mi). Perigee: 35,778 km (22,231 mi). Inclination: 0.1000 deg. Period: 1,436.10 min. Return to flight of Ariane 5 EC-A after booster failure on first launch. Delayed from April, June, September 28, October 28, November 3 and 8, 2004; and February 11, 2005. XTAR-EUR was a Spanish X-band military communications satellite operated by Hisdesat/XTAR of Spain. It had a dry mass of 1412 kg and 2219 kg of propellant. As of 2007 Mar 8 located at 28.95E drifting at 0.006W degrees per day.
2006 March 11 - .
22:33 GMT - .
Launch Site:
Kourou.
Launch Complex:
Kourou ELA3.
LV Family:
Ariane 5.
Launch Vehicle:
Ariane 5ECA.
LV Configuration: Ariane 5ECA V170 (527).
- Spainsat - .
Payload: LS-1300. Mass: 3,683 kg (8,119 lb). Nation: Spain. Agency: Hisdesat. Manufacturer: Palo Alto. Class: Communications. Type: Civilian communications satellite. Spacecraft: FS-1300. USAF Sat Cat: 28945 . COSPAR: 2006-007A. Apogee: 35,797 km (22,243 mi). Perigee: 35,777 km (22,230 mi). Inclination: 0.0000 deg. Period: 1,436.10 min. Summary: Spainsat was to provide secure X and Ku band communications for the Spanish defense ministry. It had a dry mass of 1467 kg and a solar panel span of 31.4m. As of 2007 Mar 10 located at 29.99W drifting at 0.010W degrees per day..
2009 July 29 - .
18:46 GMT - .
Launch Site:
Baikonur.
Launch Complex:
Baikonur LC109.
LV Family:
R-36M.
Launch Vehicle:
Dnepr.
- Deimos 1 - .
Mass: 90 kg (198 lb). Nation: Spain. Agency: Makeyev. Spacecraft: MicroSat-100. USAF Sat Cat: 35681 . COSPAR: 2009-041A. Apogee: 677 km (420 mi). Perigee: 635 km (394 mi). Inclination: 98.1000 deg. Period: 97.80 min. Summary: Deimos Space SL, Madrid, Spain..
- Nanosat 1B - .
Mass: 22 kg (48 lb). Nation: Spain. Agency: Makeyev. USAF Sat Cat: 35685 . COSPAR: 2009-041E. Apogee: 677 km (420 mi). Perigee: 587 km (364 mi). Inclination: 98.1000 deg. Period: 97.30 min. Summary: INTA, Spain..
2010 December 29 - .
21:27 GMT - .
Launch Site:
Kourou.
Launch Complex:
Kourou ELA3.
LV Family:
Ariane 5.
Launch Vehicle:
Ariane 5ECA.
LV Configuration: Ariane 5ECA s/n V199.
- Hispasat 1E - .
Mass: 5,320 kg (11,720 lb). Nation: Spain. Agency: Hispasat. Program: Hispasat. Class: Communications. Type: Communications satellite. Spacecraft: FS-1300. USAF Sat Cat: 37264 . COSPAR: 2010-070A. Apogee: 35,790 km (22,230 mi). Perigee: 35,785 km (22,235 mi). Inclination: 0.0000 deg. Period: 1,436.10 min. Summary: Ku band communications; 5320 kg loaded / 2175 kg unfuelled..
Home - Browse - Contact
© / Conditions for Use
