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 (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: 7 hours ago

TLE from 7 hours ago
0 SPACEMOBILE-SSR03 DEB
1 62371U 24163H   26093.63302570  .00031165  00000-0  83010-3 0  9992
2 62371  52.9694 264.0150 0007801 272.2676  87.7432 15.37910761 80405
Epoch: 2026-04-03T15:11Z
TLE epoch observation values (Epoch: 2026-04-03T15:11:33.420Z)
Latitude
-0.00005°
Longitude
-155.83864°
Altitude
452.965 km
Speed
7.642 km/s
True Right ascension
17h 36m 03s
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
03:34:19
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
457.905 km
Perigee altitude
447.248 km
Semi-major axis
6,830.714 km
Eccentricity
0.00078
Inclination
52.9694°
RAAN
264.015°
Arg. of periapsis
272.2676°
True anomaly
87.83253°
Mean anomaly
87.7432°
Eccentric anomaly
87.78786°
Mean motion
3.84454 °/min
Orbital period
93.64 mins
BSTAR
0.0008301
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