SATCOM C5, 13631
Orbit data source: Space-Track
SATCOM C5, 13631 is a payload satellite owned by RCA Americom (US) in GEO that was launched on Thu, 28 Oct 1982 UTC via a DELTA 3924 launch vehicle from the Air Force Eastern Test Range (AFETR). Payloads include a variety of satellites, spacecraft, and rockets equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.
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13631 intel report (Beta)
SATCOM C5 details
| Identifier | |
| Orbit | GEO |
| Last TLE update | 1 day ago |
| Origin | |
| Manufacturer | RCA/East Windsor |
| Mission | Non-operational Commercial Communications |
| Bus & Motor | ADV SATCOM, TE-M-700-5 |
| Mass | 1,116 kg wet, 430 kg dry |
| Launch date (UTC) | |
| Launch vehicle | |
| Launch site | |
| Object type | Payload Rocket body Debris |
| Shape & HBR | Hex Poly + 2 Pan, 1.75 m |
| Radar Cross Section | 2.655 m², Large (>1 m²) |
Expand to show TLE details & history
TLE from 1 day ago
0 SATCOM C5
1 13631U 82105A 24346.00123972 -.00000108 00000-0 00000-0 0 9993
2 13631 12.7303 336.3485 0001859 335.3641 24.4194 1.00271463120823Epoch: 2024-12-11T00:01Z
Definitive object data (Epoch: 2024-12-11T00:01:47.111Z)
| Latitude | -0.04187° |
| Longitude | -104.51986° |
| Altitude | 35,779.124 km |
| Speed | 3.075 km/s |
| True Right ascension | 22h 24m 30s |
| True Declination | 0° 02' 31" |
| Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
| Latitude | 11.00577° |
| Longitude | -45.10326° |
| Altitude | 35,784.837 km |
| Speed | 3.075 km/s |
| Apparent Right ascension | 02h 22m 10s |
| Apparent Declination | 6° 12' 36" |
| Sunlit | Object is in daylight |
Visualization observer readout
| Local Sidereal Time | 02:22:15 |
| Azimuth | 180.037° SSW |
| Elevation | 56.294° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 35,795.518 km |
| Perigee altitude | 35,779.841 km |
| Semi-major axis | 42,165.817 km |
| Eccentricity | 0.0001859 |
| Inclination | 12.7303° |
| RAAN | 336.3485° |
| Arg. of periapsis | 335.3641° |
| True anomaly | 24.42821° |
| Mean anomaly | 24.4194° |
| Eccentric anomaly | 24.4238° |
| Mean motion | 0.25067 °/min |
| BSTAR | Unknown |
| Orbital period | 1436.15 mins |
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13631 neighbors
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Other satellites on launch #105 in the year 1982 (1982-10-28 UTC)
| SATCOM C5, 13631 |
| DELTA 1 R/B(1), 13632 (Decayed) |
| DELTA 1 R/B(2), 13684 (Decayed) |
SATCOM C5 Visibility forecast
Observer location: undefined°, undefined
Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
|---|---|---|---|---|---|---|---|
| 1440 mins | 2024-12-12 03:57:19.777Z | 180.037° SSW | 2024-12-12 05:59:19.777Z | 178.681° S | 40.383° | 2024-12-13 03:57:19.777Z | 180.015° SSW |
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