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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62372 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
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
Shape & HBR
Cyl, 3.8 m
Radar Cross Section
1.963 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 6 days ago
TLE from 6 days ago
0 SPACEMOBILE-SSR04 DEB
1 62372U 24163J 26153.96644048 .00016748 00000-0 42780-3 0 9994
2 62372 52.9866 338.1745 0006287 123.0414 237.1193 15.39602242 92761Epoch: 2026-06-02T23:11Z
TLE epoch observation values (Epoch: 2026-06-02T23:11:40.457Z)
Latitude
-0.00004°
Longitude
98.82407°
Altitude
450.501 km
Speed
7.642 km/s
True Right ascension
22h 32m 41s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
02:20:08
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
451.862 km
Perigee altitude
443.279 km
Semi-major axis
6,825.707 km
Eccentricity
0.00063
Inclination
52.9866°
RAAN
338.1745°
Arg. of periapsis
123.0414°
True anomaly
237.05882°
Mean anomaly
237.1193°
Eccentric anomaly
237.08906°
Mean motion
3.84877 °/min
Orbital period
93.54 mins
BSTAR
0.0004278
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Other satellites on launch #163 in the year 2024 (2024-09-12 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.SPACEMOBILE-SSR04 DEB Visibility forecast
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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 | 2026-06-08 18:17:23.121Z | 346.892° N | 2026-06-08 18:19:23.121Z | 27.052° NE | 16.438° | 2026-06-08 18:21:23.121Z | 63.485° ENE |
| 4 mins | 2026-06-08 19:55:23.121Z | 310.464° NW | 2026-06-08 19:56:23.121Z | 311.829° NW | 42.007° | 2026-06-08 19:59:23.121Z | 130.205° SE |
| 5 mins | 2026-06-09 12:43:23.121Z | 222.229° SW | 2026-06-09 12:45:23.121Z | 192.009° SSW | 42.782° | 2026-06-09 12:48:23.121Z | 54.171° ENE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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