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   26204.44617156  .00015220  00000-0  37314-3 0  9995
2 62372  52.9841  99.0954 0003034 298.2866  61.7830 15.40944178100546
Epoch: 2026-07-23T10:42Z
TLE epoch observation values (Epoch: 2026-07-23T10:42:29.222Z)
Latitude
-0.0001°
Longitude
-2.71347°
Altitude
443.228 km
Speed
7.648 km/s
True Right ascension
06h 36m 22s
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
10:36:33
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
445.677 km
Perigee altitude
441.538 km
Semi-major axis
6,821.745 km
Eccentricity
0.0003
Inclination
52.9841°
RAAN
99.0954°
Arg. of periapsis
298.2866°
True anomaly
61.81364°
Mean anomaly
61.783°
Eccentric anomaly
61.79832°
Mean motion
3.85212 °/min
Orbital period
93.45 mins
BSTAR
0.00037314
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