SPACEMOBILE-SSR03 DEB, 62371
Orbit data source: Space-Track
SPACEMOBILE-SSR03 DEB, 62371 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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62371 intel report (Beta)
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Edit Public Description
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: 11 hours ago
TLE from 11 hours ago
0 SPACEMOBILE-SSR03 DEB
1 62371U 24163H 25340.61476041 .00030357 00000-0 95237-3 0 9995
2 62371 52.9725 98.9081 0008804 259.8047 100.1960 15.32776509 62270Epoch: 2025-12-06T14:45Z
TLE epoch observation values (Epoch: 2025-12-06T14:45:15.299Z)
Latitude
0.00001°
Longitude
161.9544°
Altitude
469.485 km
Speed
7.632 km/s
True Right ascension
06h 35m 37s
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
23:31:36
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
473.847 km
Perigee altitude
461.793 km
Semi-major axis
6,845.957 km
Eccentricity
0.00088
Inclination
52.9725°
RAAN
98.9081°
Arg. of periapsis
259.8047°
True anomaly
100.29527°
Mean anomaly
100.196°
Eccentric anomaly
100.24564°
Mean motion
3.8317 °/min
Orbital period
93.95 mins
BSTAR
0.00095237
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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-SSR03 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 | 2025-12-07 09:41:45.825Z | 164.532° S | 2025-12-07 09:43:45.825Z | 122.785° SE | 18.6° | 2025-12-07 09:45:45.825Z | 86.123° E |
| 5 mins | 2025-12-07 11:18:45.825Z | 257.482° W | 2025-12-07 11:20:45.825Z | 311.197° NW | 36.228° | 2025-12-07 11:23:45.825Z | 36.947° NE |
| 4 mins | 2025-12-07 16:15:45.825Z | 348.895° N | 2025-12-07 16:17:45.825Z | 37.464° NE | 21.812° | 2025-12-07 16:19:45.825Z | 76.067° E |
| 6 mins | 2025-12-07 17:52:45.825Z | 296.558° NW | 2025-12-07 17:55:45.825Z | 194.231° SSW | 36.975° | 2025-12-07 17:58:45.825Z | 147.197° SSE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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