SPACEMOBILE-SSR04 DEB, 62372
Orbit data source: Space-Track
SPACEMOBILE-SSR04 DEB, 62372 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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Edit Public Description
Identifier | |
Orbit | LEO |
Last TLE update | 9 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, Large (>1 m²) |
Expand to show TLE details & history
TLE from 9 hours ago
0 SPACEMOBILE-SSR04 DEB
1 62372U 24163J 25070.82595687 .00017022 00000-0 70447-3 0 9997
2 62372 52.9896 272.1304 0008852 163.9631 196.1647 15.24036798 24096
Epoch: 2025-03-11T19:49Z
Definitive object data (Epoch: 2025-03-11T19:49:22.673Z)
Latitude | 0° |
Longitude | 165.06259° |
Altitude | 500.401 km |
Speed | 7.612 km/s |
True Right ascension | 18h 08m 31s |
True Declination | 0° 00' 00" |
Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
Latitude | -41.27244° |
Longitude | 24.4952° |
Altitude | 505.256 km |
Speed | 7.612 km/s |
Apparent Right ascension | 05h 23m 38s |
Apparent Declination | -86° 53' 58" |
Sunlit | Object is in full shadow |
Visualization observer readout
Local Sidereal Time | 09:03:06 |
Azimuth | 183.222° SSW |
Elevation | -38.087° |
Doppler factor | 1 |
Orbital elements
Apogee altitude | 500.046 km |
Perigee altitude | 487.879 km |
Semi-major axis | 6,872.099 km |
Eccentricity | 0.0008852 |
Inclination | 52.9896° |
RAAN | 272.1304° |
Arg. of periapsis | 163.9631° |
True anomaly | 196.13649° |
Mean anomaly | 196.1647° |
Eccentric anomaly | 196.15059° |
Mean motion | 3.80986 °/min |
BSTAR | 0.00070447 |
Orbital period | 94.49 mins |
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Other satellites on launch #163 in the year 2024 (2024-09-12 UTC)
SPACEMOBILE-SSR04 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. |
---|---|---|---|---|---|---|---|
4 mins | 2025-03-12 14:52:13.073Z | 161.303° S | 2025-03-12 14:54:13.073Z | 122.88° SE | 17.447° | 2025-03-12 14:56:13.073Z | 88.229° E |
5 mins | 2025-03-12 16:30:13.073Z | 257.613° W | 2025-03-12 16:32:13.073Z | 340.263° N | 38.809° | 2025-03-12 16:35:13.073Z | 41.154° NE |
4 mins | 2025-03-12 21:28:13.073Z | 344.982° N | 2025-03-12 21:30:13.073Z | 29.264° NE | 21.882° | 2025-03-12 21:32:13.073Z | 70.496° E |
6 mins | 2025-03-12 23:06:13.073Z | 297.796° NW | 2025-03-12 23:08:13.073Z | 256.094° W | 38.892° | 2025-03-12 23:12:13.073Z | 144.5° SSE |
Event ID | Pc | Md | Secondary | Secondary name | Country | Click to unsort rows by TCA header |
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