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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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: 14 hours ago
TLE from 14 hours ago
0 SPACEMOBILE-SSR02 DEB
1 62370U 24163G 26253.34745813 .00018761 00000-0 38861-3 0 9999
2 62370 52.9398 218.8561 0008546 95.9440 264.2539 15.45787253111529Epoch: 2026-09-10T08:20Z
TLE epoch observation values (Epoch: 2026-09-10T08:20:20.382Z)
Latitude
-0.00001°
Longitude
104.3847°
Altitude
430.535 km
Speed
7.654 km/s
True Right ascension
14h 35m 25s
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
14:49:39
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
435.178 km
Perigee altitude
423.542 km
Semi-major axis
6,807.497 km
Eccentricity
0.00085
Inclination
52.9398°
RAAN
218.8561°
Arg. of periapsis
95.944°
True anomaly
264.15647°
Mean anomaly
264.2539°
Eccentric anomaly
264.20519°
Mean motion
3.86422 °/min
Orbital period
93.16 mins
BSTAR
0.00038861
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-09-11 00:01:15.808Z | 199.245° SSW | 2026-09-11 00:04:15.808Z | 114.516° SE | 35.979° | 2026-09-11 00:06:15.808Z | 70.392° E |
| 4 mins | 2026-09-11 01:39:15.808Z | 289.882° WNW | 2026-09-11 01:41:15.808Z | 345.407° N | 25.108° | 2026-09-11 01:43:15.808Z | 25.602° NE |
| 4 mins | 2026-09-11 06:33:15.808Z | 347.774° N | 2026-09-11 06:34:15.808Z | 18.788° NNE | 32.875° | 2026-09-11 06:37:15.808Z | 95.718° ESE |
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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