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: 20 hours ago

TLE from 20 hours ago
0 SPACEMOBILE-SSR03 DEB
1 62371U 24163H   26284.14652080  .00029475  00000-0  62902-3 0  9992
2 62371  52.9679  80.1230 0007609 160.2889 199.8411 15.44633614109784
Epoch: 2026-10-11T03:30Z
TLE epoch observation values (Epoch: 2026-10-11T03:30:59.397Z)
Latitude
0°
Longitude
7.63203°
Altitude
438.214 km
Speed
7.647 km/s
True Right ascension
05h 20m 29s
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
18:02:52
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
437.926 km
Perigee altitude
427.562 km
Semi-major axis
6,810.881 km
Eccentricity
0.00076
Inclination
52.9679°
RAAN
80.123°
Arg. of periapsis
160.2889°
True anomaly
199.81153°
Mean anomaly
199.8411°
Eccentric anomaly
199.82631°
Mean motion
3.86134 °/min
Orbital period
93.23 mins
BSTAR
0.00062902
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