SPACEMOBILE-SSR01 DEB, 62369
Orbit data source: Space-Track
SPACEMOBILE-SSR01 DEB, 62369 is space debris in LEO originally from a launch on Thu, 12 Sep 2024 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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62369 intel report (Beta)
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Edit Public Description
Identifier | |
Orbit | LEO |
Last TLE update | 6 hours ago |
Origin | |
Manufacturer | AST & Science |
Mission | Spacecraft |
Bus & Motor | BW3 LVA, Unknown motor |
Mass | 150 kg wet, 150 kg dry |
Launch date (UTC) | |
Launch vehicle | Unknown |
Launch site | |
Object type | Payload Rocket body Debris |
Shape & HBR | Cyl, 2 m |
Radar Cross Section | 1.963 m², Medium (>0.1 m² and < 1m²) |
Expand to show TLE details & history
TLE from 6 hours ago
0 SPACEMOBILE-SSR01 DEB
1 62369U 24163F 25070.95369080 .00016743 00000-0 69839-3 0 9995
2 62369 53.0004 272.1678 0011579 157.2395 202.9116 15.23760604 15762
Epoch: 2025-03-11T22:53Z
Definitive object data (Epoch: 2025-03-11T22:53:18.885Z)
Latitude | -0.00004° |
Longitude | 118.98985° |
Altitude | 502.721 km |
Speed | 7.61 km/s |
True Right ascension | 18h 08m 40s |
True Declination | 0° 00' 00" |
Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
Latitude | -43.28972° |
Longitude | -17.21402° |
Altitude | 507.717 km |
Speed | 7.611 km/s |
Apparent Right ascension | 11h 42m 50s |
Apparent Declination | -88° 57' 53" |
Sunlit | Object is in full shadow |
Visualization observer readout
Local Sidereal Time | 08:59:06 |
Azimuth | 179.126° S |
Elevation | -39.131° |
Doppler factor | 1 |
Orbital elements
Apogee altitude | 502.749 km |
Perigee altitude | 486.833 km |
Semi-major axis | 6,872.928 km |
Eccentricity | 0.0011579 |
Inclination | 53.0004° |
RAAN | 272.1678° |
Arg. of periapsis | 157.2395° |
True anomaly | 202.86001° |
Mean anomaly | 202.9116° |
Eccentric anomaly | 202.8858° |
Mean motion | 3.80917 °/min |
BSTAR | 0.00069839 |
Orbital period | 94.51 mins |
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Other satellites on launch #163 in the year 2024 (2024-09-12 UTC)
SPACEMOBILE-SSR01 DEB 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. |
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4 mins | 2025-03-12 14:47:14.568Z | 157.404° SSE | 2025-03-12 14:49:14.568Z | 122.159° SE | 15.122° | 2025-03-12 14:51:14.568Z | 89.95° E |
6 mins | 2025-03-12 16:24:14.568Z | 243.86° WSW | 2025-03-12 16:27:14.568Z | 350.372° N | 41.046° | 2025-03-12 16:30:14.568Z | 43.826° NE |
4 mins | 2025-03-12 21:23:14.568Z | 346.416° N | 2025-03-12 21:25:14.568Z | 28.955° NE | 20.233° | 2025-03-12 21:27:14.568Z | 67.748° E |
6 mins | 2025-03-12 23:01:14.568Z | 302.498° NW | 2025-03-12 23:03:14.568Z | 270.698° WNW | 41.023° | 2025-03-12 23:07:14.568Z | 139.35° SSE |
Event ID | Pc | Md | Secondary | Secondary name | Country | Click to unsort rows by TCA header |
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