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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Identifier
62371, 2024-163H
Orbit
LEO
Country
Flag of USUS
Related business
Manufacturer
AST & Science
Mission
Spacecraft
Bus & Motor
BW3 LVA, Unknown motor
Mass
150 kg wet, 150 kg dry
Launch date (UTC)
2024-09-12 (2 years ago)
Launch vehicle
Unknown
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl, 3.8 m
Radar Cross Section
1.963 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 9 hours ago

TLE from 9 hours ago
0 SPACEMOBILE-SSR03 DEB
1 62371U 24163H   26235.59081384  .00016072  00000-0  36874-3 0  9998
2 62371  52.9706 311.3636 0008578  15.7011 344.4257 15.42875111102283
Epoch: 2026-08-23T14:10Z
TLE epoch observation values (Epoch: 2026-08-23T14:10:46.315Z)
Latitude
-0.00005°
Longitude
126.7859°
Altitude
432.882 km
Speed
7.656 km/s
True Right ascension
20h 45m 27s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
13:58:58
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
443.764 km
Perigee altitude
432.071 km
Semi-major axis
6,816.054 km
Eccentricity
0.00086
Inclination
52.9706°
RAAN
311.3636°
Arg. of periapsis
15.7011°
True anomaly
344.39928°
Mean anomaly
344.4257°
Eccentric anomaly
344.41249°
Mean motion
3.85695 °/min
Orbital period
93.34 mins
BSTAR
0.00036874
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