SPACEMOBILE-SSR04 DEB, 62372

Orbit data source: Space-Track

SPACEMOBILE-SSR04 DEB, 62372 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
62372, 2024-163J
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-SSR04 DEB
1 62372U 24163J   25241.15939747  .00016871  00000-0  61164-3 0  9999
2 62372  52.9893 202.0090 0005962 357.6460   2.4508 15.28472551 50110
Epoch: 2025-08-29T03:49Z
TLE epoch observation values (Epoch: 2025-08-29T03:49:31.941Z)
Latitude
-0.00007°
Longitude
167.01381°
Altitude
477.173 km
Speed
7.631 km/s
True Right ascension
13h 28m 02s
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
14:26:20
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
484.751 km
Perigee altitude
476.572 km
Semi-major axis
6,858.799 km
Eccentricity
0.0006
Inclination
52.9893°
RAAN
202.009°
Arg. of periapsis
357.646°
True anomaly
2.45372°
Mean anomaly
2.4508°
Eccentric anomaly
2.45226°
Mean motion
3.82095 °/min
Orbital period
94.22 mins
BSTAR
0.00061164
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