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 (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: 11 hours ago

TLE from 11 hours ago
0 SPACEMOBILE-SSR04 DEB
1 62372U 24163J   26199.77619228  .00008038  00000-0  20262-3 0  9999
2 62372  52.9845 121.2315 0002796 280.4095  79.6593 15.40827213 99822
Epoch: 2026-07-18T18:37Z
TLE epoch observation values (Epoch: 2026-07-18T18:37:43.012Z)
Latitude
-0.00004°
Longitude
-94.78184°
Altitude
444.21 km
Speed
7.647 km/s
True Right ascension
08h 04m 55s
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
18:48:49
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
445.86 km
Perigee altitude
442.045 km
Semi-major axis
6,822.09 km
Eccentricity
0.00028
Inclination
52.9845°
RAAN
121.2315°
Arg. of periapsis
280.4095°
True anomaly
79.69082°
Mean anomaly
79.6593°
Eccentric anomaly
79.67506°
Mean motion
3.85183 °/min
Orbital period
93.46 mins
BSTAR
0.00020262
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