GOES-5, known as GOES-E before becoming operational, was a geostationary weather satellite which was operated by the United States National Oceanic and Atmospheric Administration as part of the Geostationary Operational Environmental Satellite system.[1] Launched in 1981, it was used for weather forecasting in the United States.
![]() Artist's impression of an HS-371 derived GOES satellite | |
Mission type | Weather satellite |
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Operator | NOAA / NASA |
COSPAR ID | 1981-049A ![]() |
SATCAT no. | 12472 |
Mission duration | 7 years (planned) 3 years (VISSR) 9 years (total) |
Spacecraft properties | |
Bus | HS-371 |
Manufacturer | Hughes |
Launch mass | 660 kilograms (1,460 lb) |
Start of mission | |
Launch date | 22 May 1981, 22:29 (1981-05-22UTC22:29Z) UTC |
Rocket | Delta 3914 |
Launch site | Cape Canaveral LC-17A |
Contractor | McDonnell Douglas |
End of mission | |
Disposal | Decommissioned |
Deactivated | 18 July 1990 (1990-07-19) |
Orbital parameters | |
Reference system | Geocentric |
Regime | Geostationary |
Longitude | 85° West (1981) 75° West (1981-1987) 106° West (1987-1988) 65° West (1988-1989) |
Slot | GOES-EAST (1981-1987) |
Semi-major axis | 42,146.0 kilometers (26,188.3 mi) |
Perigee altitude | 35,749.8 kilometers (22,213.9 mi) |
Apogee altitude | 35,801.1 kilometers (22,245.8 mi) |
Inclination | 14.6 degrees |
Period | 1,435.2 minutes |
GOES-5 was built by Hughes Space and Communications, and was based on the HS-371 satellite bus. At launch it had a mass of 660 kilograms (1,460 lb),[2] with an expected operational lifespan of around seven years.
GOES-E was launched using a Delta 3914 carrier rocket[3] flying from Launch Complex 17A at the Cape Canaveral Air Force Station.[4] The launch occurred at 22:29 GMT on 22 May 1981.[5] The launch successfully placed GOES-E into a geostationary transfer orbit, from which it raised itself to geostationary orbit on 2 June by means of an onboard Star 27 apogee motor.[3][6]
Following insertion into geostationary orbit, GOES-5 was briefly placed at a longitude 85° West, however by the end of 1981, it had been moved to 75° West. It remained there until 1987, when it was moved to 106° West. In 1988 it was relocated to 65° West, where it operated until 1989.[4] The primary instrument carried aboard GOES-5, the Visible Infrared Spin-Scan Radiometer or VISSR, failed in 1984.[2] The GOES-1 and GOES-4 satellites were reactivated to fill the gap in coverage until a replacement could be launched. It was finally replaced by the ground spare, GOES-H, in 1987 after its intended replacement, GOES-G, failed to reach orbit. GOES-5 was retired to a graveyard orbit on 18 July 1990.[1][6]
Geostationary Operational Environmental Satellites | ||
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SMS (predecessor) |
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SMS derived | ||
1st generation | ||
2nd generation | ||
3rd generation | ||
4th generation | ||
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← 1980 · Orbital launches in 1981 · 1982 → | |
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Kosmos 1237 | Molniya-3 No.25 | Kosmos 1238 | Kosmos 1239 | Kosmos 1240 | Kosmos 1241 | Musson No.11 | Progress 12 | Kosmos 1242 | Molniya 1-49 | Kosmos 1243 | Interkosmos 21 | Kiku 3 | Kosmos 1244 | Kosmos 1245 | Kosmos 1246 | Kosmos 1247 | Hinotori | Comstar D4 | OPS 1166 | Kosmos 1248 | Kosmos 1249 | Kosmos 1250 · Kosmos 1251 · Kosmos 1252 · Kosmos 1253 · Kosmos 1254 · Kosmos 1255 · Kosmos 1256 · Kosmos 1257 | Soyuz T-4 | Kosmos 1258 | OPS 7350 | Kosmos 1259 | Gran' No.18L | Kosmos 1260 | Soyuz 39 | Molniya-3 No.24 | Yantar-2K No.979 | Kosmos 1261 | Kosmos 1262 | Kosmos 1263 | STS-1 | Kosmos 1264 | Kosmos 1265 | Kosmos 1266 | OPS 7225 | Kosmos 1267 | Kosmos 1268 | Kosmos 1269 | Soyuz 40 | Meteor-2 No.8 | Nova-1 | Kosmos 1270 | Kosmos 1271 | Kosmos 1272 | Kosmos 1273 | GOES 5 | Intelsat V F-1 | Rohini RS-D1 | Kosmos 1274 | Kosmos 1275 | Molniya-3 No.30 | Kosmos 1276 | Kosmos 1277 | Meteosat 2 · APPLE · CAT-3 | Kosmos 1278 | NOAA-7 | Molniya 1-50 | Ekran No.21L | Kosmos 1279 | Kosmos 1280 | Kosmos 1281 | Meteor-Priroda 2-4 · Iskra 1 | Kosmos 1282 | Kosmos 1283 | Kosmos 1284 | Gran' No.19L | DE-1 · DE-2 | Kosmos 1285 | Kosmos 1286 | FLTSATCOM 5 | Kosmos 1287 · Kosmos 1288 · Kosmos 1289 · Kosmos 1290 · Kosmos 1291 · Kosmos 1292 · Kosmos 1293 · Kosmos 1294 | Bulgaria 1300 | Himawari 2 | Kosmos 1295 | Kosmos 1296 | Kosmos 1297 | Kosmos 1298 | Kosmos 1299 | Kosmos 1300 | Kosmos 1301 | Kosmos 1302 | OPS 3984 | Kosmos 1303 | Kosmos 1304 | Kosmos 1305 | Kosmos 1306 | Kosmos 1307 | Kosmos 1308 | Kosmos 1309 | Shijian 2 · Shijian 2-01 · Shijian 2-02 | Oreol 3 | Kosmos 1310 | SBS 2 | Kosmos 1311 | Kosmos 1312 | Kosmos 1313 | SME · UoSAT-1 | Kosmos 1314 | Gran' No.20L | Kosmos 1315 | Kosmos 1316 | Molniya-3 No.31 | Venera 13 | OPS 4029 | Kosmos 1317 | Kosmos 1318 | Venera 14 | STS-2 | Kosmos 1319 | Molniya 1-51 | Satcom 3R | Bhaskara 2 | Kosmos 1320 · Kosmos 1321 · Kosmos 1322 · Kosmos 1323 · Kosmos 1324 · Kosmos 1325 · Kosmos 1326 · Kosmos 1327 | Kosmos 1328 | Kosmos 1329 | Intelsat V F-3 | RS-3 · RS-4 · RS-5 · RS-6 · RS-7 · RS-8 | Navstar 7 | Kosmos 1330 | MARECS-1 · CAT-4 | Molniya-1 No.55 | |
Payloads are separated by bullets ( · ), launches by pipes ( | ). Crewed flights are indicated in underline. Uncatalogued launch failures are listed in italics. Payloads deployed from other spacecraft are denoted in (brackets). |