SPACEMOBILE-SSR02 DEB, 62370
Orbit data source: Space-Track
SPACEMOBILE-SSR02 DEB, 62370 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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62370 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-SSR02 DEB
1 62370U 24163G 25288.55619819 .00021986 00000-0 72247-3 0 9994
2 62370 52.9473 339.5901 0009118 117.1667 243.0262 15.31470204 60730Epoch: 2025-10-15T13:20Z
TLE epoch observation values (Epoch: 2025-10-15T13:20:55.523Z)
Latitude
-0.00003°
Longitude
115.03015°
Altitude
475.14 km
Speed
7.628 km/s
True Right ascension
22h 38m 21s
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
18:36:34
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
477.962 km
Perigee altitude
465.47 km
Semi-major axis
6,849.853 km
Eccentricity
0.00091
Inclination
52.9473°
RAAN
339.5901°
Arg. of periapsis
117.1667°
True anomaly
242.93313°
Mean anomaly
243.0262°
Eccentric anomaly
242.97966°
Mean motion
3.82844 °/min
Orbital period
94.03 mins
BSTAR
0.00072247
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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-SSR02 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 | 2025-10-16 05:09:59.160Z | 168.955° S | 2025-10-16 05:11:59.160Z | 131.693° SE | 17.775° | 2025-10-16 05:13:59.160Z | 92.265° ESE |
| 5 mins | 2025-10-16 06:47:59.160Z | 261.614° W | 2025-10-16 06:49:59.160Z | 344.408° N | 36.737° | 2025-10-16 06:52:59.160Z | 40.785° NE |
| 4 mins | 2025-10-16 11:44:59.160Z | 355.217° N | 2025-10-16 11:45:59.160Z | 19.04° NNE | 21.354° | 2025-10-16 11:48:59.160Z | 78.991° E |
| 5 mins | 2025-10-16 13:21:59.160Z | 296.025° NW | 2025-10-16 13:23:59.160Z | 246.757° WSW | 38.478° | 2025-10-16 13:26:59.160Z | 149.028° 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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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