SPACEMOBILE-SSR01 DEB, 62369
Orbit data source: Space-Track
SPACEMOBILE-SSR01 DEB, 62369 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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62369 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: 15 hours ago
TLE from 15 hours ago
0 SPACEMOBILE-SSR01 DEB
1 62369U 24163F 25340.45031752 .00017319 00000-0 59142-3 0 9998
2 62369 52.9954 101.4259 0007430 279.3719 80.6440 15.30402239 56941Epoch: 2025-12-06T10:48Z
TLE epoch observation values (Epoch: 2025-12-06T10:48:27.433Z)
Latitude
0.00001°
Longitude
-136.16628°
Altitude
474.669 km
Speed
7.63 km/s
True Right ascension
06h 45m 42s
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
23:28:34
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
479.986 km
Perigee altitude
469.803 km
Semi-major axis
6,853.031 km
Eccentricity
0.00074
Inclination
52.9954°
RAAN
101.4259°
Arg. of periapsis
279.3719°
True anomaly
80.72802°
Mean anomaly
80.644°
Eccentric anomaly
80.68601°
Mean motion
3.82577 °/min
Orbital period
94.1 mins
BSTAR
0.00059142
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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-SSR01 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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-12-07 10:28:43.748Z | 210.392° SW | 2025-12-07 10:31:43.748Z | 152.984° SSE | 37.082° | 2025-12-07 10:34:43.748Z | 63.555° ENE |
| 4 mins | 2025-12-07 12:08:43.748Z | 299.216° NW | 2025-12-07 12:09:43.748Z | 323.043° NNW | 22.595° | 2025-12-07 12:12:43.748Z | 25.854° NE |
| 5 mins | 2025-12-07 17:04:43.748Z | 328.435° NNW | 2025-12-07 17:06:43.748Z | 22.538° NE | 35.679° | 2025-12-07 17:09:43.748Z | 105.454° 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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