S80/T, 22078
Orbit data source: Space-Track
S80/T, 22078 is a payload satellite owned by CNES (FR) in LEO that was launched on Mon, 10 Aug 1992 UTC via an ARIANE 42P launch vehicle from the French Guiana (FRGUI). 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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22078 intel report (Beta)
S80/T details
| Identifier | |
| Orbit | LEO |
| Last TLE update | 1 day ago |
| Origin | |
| Manufacturer | SSTL/MMST |
| Mission | Civil Communications |
| Bus & Motor | UOSAT, Unknown motor |
| Mass | 50 kg wet, 50 kg dry |
| Launch date (UTC) | |
| Launch vehicle | |
| Launch site | |
| Object type | Payload Rocket body Debris |
| Shape & HBR | Hex Poly, 0.7 m |
| Radar Cross Section | 0.140 m², Medium (>0.1 m² and < 1m²) |
Expand to show TLE details & history
TLE from 1 day ago
0 S80/T
1 22078U 92052C 24360.28414578 -.00000032 00000-0 12065-3 0 9994
2 22078 66.0861 317.9099 0012024 219.2477 140.7671 12.86835378520898Epoch: 2024-12-25T06:49Z
Definitive object data (Epoch: 2024-12-25T06:49:10.195Z)
| Latitude | -0.00001° |
| Longitude | 121.33731° |
| Altitude | 1,323.198 km |
| Speed | 7.193 km/s |
| True Right ascension | 21h 11m 38s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
| Latitude | -8.18664° |
| Longitude | 115.25964° |
| Altitude | 1,323.702 km |
| Speed | 7.192 km/s |
| Apparent Right ascension | 21h 18m 09s |
| Apparent Declination | -22° 41' 20" |
| Sunlit | Object is in daylight |
Visualization observer readout
| Local Sidereal Time | 10:06:20 |
| Azimuth | 34.218° NE |
| Elevation | -69.977° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 1,321.91 km |
| Perigee altitude | 1,303.415 km |
| Semi-major axis | 7,690.8 km |
| Eccentricity | 0.0012024 |
| Inclination | 66.0861° |
| RAAN | 317.9099° |
| Arg. of periapsis | 219.2477° |
| True anomaly | 140.85414° |
| Mean anomaly | 140.7671° |
| Eccentric anomaly | 140.81063° |
| Mean motion | 3.218 °/min |
| BSTAR | 0.00012065 |
| Orbital period | 111.87 mins |
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Other satellites on launch #52 in the year 1992 (1992-08-10 UTC)
S80/T 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. |
|---|---|---|---|---|---|---|---|
| 14 mins | 2024-12-26 22:05:05.959Z | 179.671° S | 2024-12-26 22:12:05.959Z | 108.009° ESE | 36.468° | 2024-12-26 22:19:05.959Z | 41.791° NE |
| 13 mins | 2024-12-27 00:01:05.959Z | 246.099° WSW | 2024-12-27 00:07:05.959Z | 305.148° NW | 33.472° | 2024-12-27 00:14:05.959Z | 16.856° NNE |
| 5 mins | 2024-12-27 02:03:05.959Z | 319.112° NNW | 2024-12-27 02:05:05.959Z | 334.557° NNW | 12.863° | 2024-12-27 02:08:05.959Z | 357.662° N |
| 10 mins | 2024-12-27 06:00:05.959Z | 358.096° N | 2024-12-27 06:04:05.959Z | 34.175° NE | 21.937° | 2024-12-27 06:10:05.959Z | 86.462° E |
| 14 mins | 2024-12-27 07:54:05.959Z | 330.306° NNW | 2024-12-27 08:01:05.959Z | 102.897° ESE | 44.976° | 2024-12-27 08:08:05.959Z | 151.106° SSE |
| 8 mins | 2024-12-27 09:52:05.959Z | 285.833° WNW | 2024-12-27 09:55:05.959Z | 260.469° W | 17.111° | 2024-12-27 10:00:05.959Z | 220.696° SW |
Authenticating...
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