Encyclopedia Astronautica
Spain



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El Arenosillo
Credit: © Mark Wade
Spain

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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..

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