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, 3.8 m
Radar Cross Section
1.963 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 13 hours ago

TLE from 13 hours ago
0 SPACEMOBILE-SSR03 DEB
1 62371U 24163H   25288.47717446  .00016484  00000-0  56125-3 0  9995
2 62371  52.9756 342.6584 0010988  89.6857 270.5400 15.30507116 54282
Epoch: 2025-10-15T11:27Z
TLE epoch observation values (Epoch: 2025-10-15T11:27:07.873Z)
Latitude
-0.00006°
Longitude
146.62486°
Altitude
475.116 km
Speed
7.63 km/s
True Right ascension
22h 50m 38s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow 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
18:36:33
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
482.114 km
Perigee altitude
467.055 km
Semi-major axis
6,852.722 km
Eccentricity
0.0011
Inclination
52.9756°
RAAN
342.6584°
Arg. of periapsis
89.6857°
True anomaly
270.41409°
Mean anomaly
270.54°
Eccentric anomaly
270.47705°
Mean motion
3.82603 °/min
Orbital period
94.09 mins
BSTAR
0.00056125
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