SPACEMOBILE-SSR01 DEB, 62369

Orbit data source: Space-Track

SPACEMOBILE-SSR01 DEB, 62369 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
62369, 2024-163F
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: 23 hours ago

TLE from 23 hours ago
0 SPACEMOBILE-SSR01 DEB
1 62369U 24163F   26185.30809671  .00012443  00000-0  36888-3 0  9998
2 62369  52.9921 198.6868 0006242 212.7249 147.3366 15.35228048 89132
Epoch: 2026-07-04T07:23Z
TLE epoch observation values (Epoch: 2026-07-04T07:23:39.555Z)
Latitude
-0.00002°
Longitude
165.44832°
Altitude
464.721 km
Speed
7.633 km/s
True Right ascension
13h 14m 44s
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
18:00:33
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
464.796 km
Perigee altitude
456.259 km
Semi-major axis
6,838.664 km
Eccentricity
0.00062
Inclination
52.9921°
RAAN
198.6868°
Arg. of periapsis
212.7249°
True anomaly
147.37518°
Mean anomaly
147.3366°
Eccentric anomaly
147.35589°
Mean motion
3.83783 °/min
Orbital period
93.8 mins
BSTAR
0.00036888
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