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   26235.61734803  .00007063  00000-0  20906-3 0  9998
2 62369  52.9946 322.1584 0008326  26.1722 333.9698 15.36006965 96868
Epoch: 2026-08-23T14:48Z
TLE epoch observation values (Epoch: 2026-08-23T14:48:58.869Z)
Latitude
-0.00007°
Longitude
128.00223°
Altitude
453.702 km
Speed
7.644 km/s
True Right ascension
21h 28m 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
13:59:16
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
463.907 km
Perigee altitude
452.523 km
Semi-major axis
6,836.352 km
Eccentricity
0.00083
Inclination
52.9946°
RAAN
322.1584°
Arg. of periapsis
26.1722°
True anomaly
333.92789°
Mean anomaly
333.9698°
Eccentric anomaly
333.94885°
Mean motion
3.83978 °/min
Orbital period
93.76 mins
BSTAR
0.00020906
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