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 (1 year ago)
Launch vehicle
Unknown
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl, 1.0 m
Radar Cross Section
1.963 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 19 hours ago

TLE from 19 hours ago
0 SPACEMOBILE-SSR03 DEB
1 62371U 24163H   25241.16902273  .00019292  00000-0  69340-3 0  9997
2 62371  52.9741 203.1240 0008677 319.5317  40.5034 15.28642905 47041
Epoch: 2025-08-29T04:03Z
TLE epoch observation values (Epoch: 2025-08-29T04:03:23.563Z)
Latitude
-0.00008°
Longitude
164.65422°
Altitude
476.225 km
Speed
7.631 km/s
True Right ascension
13h 32m 29s
True Declination
0° 00' 00"
Sunlit
Object was in daylight 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
14:26:38
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
486.105 km
Perigee altitude
474.204 km
Semi-major axis
6,858.292 km
Eccentricity
0.00087
Inclination
52.9741°
RAAN
203.124°
Arg. of periapsis
319.5317°
True anomaly
40.56803°
Mean anomaly
40.5034°
Eccentric anomaly
40.53571°
Mean motion
3.82137 °/min
Orbital period
94.21 mins
BSTAR
0.0006934
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