ATLAS CENTAUR R/B, 10025
Orbit data source: Space-Track
ATLAS CENTAUR R/B, 10025 is space debris in HEO originally from a launch on Thu, 26 May 1977 UTC launched from the Air Force Eastern Test Range (AFETR). Debris objects in space refer to the collection of defunct objects orbiting the Earth. Examples of debris include non-operational satellites, rocket bodies, and fragments generated from explosions, collisions, or faulty payload assembly.
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10025 intel report (Beta)
ATLAS CENTAUR R/B details
| Identifier | |
| Orbit | HEO |
| Last TLE update | 21 hours ago |
| Origin | |
| Manufacturer | GD/Convair |
| Mission | Spacecraft |
| Bus & Motor | CENTAUR, Unknown motor |
| Mass | ~1,800 kg wet, ~1,800 kg dry |
| Launch date (UTC) | |
| Launch vehicle | Unknown |
| Launch site | |
| Object type | Payload Rocket body Debris |
| Shape & HBR | Cyl, 9.1 m |
| Radar Cross Section | 25.930 m², Large (>1 m²) |
Expand to show TLE details & history
TLE from 21 hours ago
0 ATLAS CENTAUR R/B
1 10025U 77041B 25035.29673203 -.00000098 00000-0 -59317-3 0 9991
2 10025 21.7545 67.9273 7192964 186.8594 350.1971 2.22859029386908Epoch: 2025-02-04T07:07Z
Definitive object data (Epoch: 2025-02-04T07:07:17.647Z)
| Latitude | 19.2935° |
| Longitude | -54.40305° |
| Altitude | 3,183.426 km |
| Speed | 8.203 km/s |
| True Right ascension | 12h 28m 29s |
| True Declination | 19° 12' 49" |
| Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
| Latitude | 19.58862° |
| Longitude | -111.085° |
| Altitude | 13,267.441 km |
| Speed | 4.948 km/s |
| Apparent Right ascension | 09h 30m 36s |
| Apparent Declination | 9° 22' 46" |
| Sunlit | Object is in full shadow |
Visualization observer readout
| Local Sidereal Time | 05:58:23 |
| Azimuth | 107.956° ESE |
| Elevation | 34.016° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 36,195.42 km |
| Perigee altitude | 572.701 km |
| Semi-major axis | 24,762.197 km |
| Eccentricity | 0.7192964 |
| Inclination | 21.7545° |
| RAAN | 67.9273° |
| Arg. of periapsis | 186.8594° |
| True anomaly | 290.93645° |
| Mean anomaly | 350.1971° |
| Eccentric anomaly | 328.92446° |
| Mean motion | 0.55701 °/min |
| BSTAR | -0.00059317 |
| Orbital period | 646.31 mins |
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Other satellites on launch #41 in the year 1977 (1977-05-26 UTC)
| INTELSAT 4A-F4, 10024 |
| ATLAS CENTAUR R/B, 10025 |
ATLAS CENTAUR R/B 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. |
|---|---|---|---|---|---|---|---|
| 26 mins | 2025-02-05 03:56:37.979Z | 108.001° ESE | 2025-02-05 03:56:37.979Z | 108.001° ESE | 29.211° | 2025-02-05 04:22:37.979Z | 91.939° ESE |
| 112 mins | 2025-02-05 23:14:37.979Z | 94.33° ESE | 2025-02-06 00:21:37.979Z | 93.214° ESE | 13.444° | 2025-02-06 01:06:37.979Z | 87.946° E |
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