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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Identifier
62370, 2024-163G
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: 18 hours ago

TLE from 18 hours ago
0 SPACEMOBILE-SSR02 DEB
1 62370U 24163G   25241.20822338  .00020613  00000-0  72418-3 0  9993
2 62370  52.9473 200.6566 0009101 355.1587   4.9321 15.29342858 53486
Epoch: 2025-08-29T04:59Z
TLE epoch observation values (Epoch: 2025-08-29T04:59:50.5Z)
Latitude
-0.00001°
Longitude
148.03601°
Altitude
472.436 km
Speed
7.634 km/s
True Right ascension
13h 22m 37s
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
14:26:19
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
484.306 km
Perigee altitude
471.826 km
Semi-major axis
6,856.203 km
Eccentricity
0.00091
Inclination
52.9473°
RAAN
200.6566°
Arg. of periapsis
355.1587°
True anomaly
4.94108°
Mean anomaly
4.9321°
Eccentric anomaly
4.93659°
Mean motion
3.82312 °/min
Orbital period
94.16 mins
BSTAR
0.00072418
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