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: 8 hours ago

TLE from 8 hours ago
0 SPACEMOBILE-SSR01 DEB
1 62369U 24163F   26139.92089944  .00006479  00000-0  20306-3 0  9998
2 62369  52.9945  51.8063 0009751  78.4122 281.7973 15.34326267 82164
Epoch: 2026-05-19T22:06Z
TLE epoch observation values (Epoch: 2026-05-19T22:06:05.711Z)
Latitude
0.00001°
Longitude
-157.30536°
Altitude
462.448 km
Speed
7.637 km/s
True Right ascension
03h 27m 13s
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
15:16:26
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
469.877 km
Perigee altitude
456.535 km
Semi-major axis
6,841.343 km
Eccentricity
0.00098
Inclination
52.9945°
RAAN
51.8063°
Arg. of periapsis
78.4122°
True anomaly
281.68789°
Mean anomaly
281.7973°
Eccentric anomaly
281.7426°
Mean motion
3.83558 °/min
Orbital period
93.86 mins
BSTAR
0.00020306
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