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 (1 year ago)
Launch vehicle
Unknown
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl, 1.0 m
Radar Cross Section
1.963 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 19 hours ago

TLE from 19 hours ago
0 SPACEMOBILE-SSR01 DEB
1 62369U 24163F   25241.15818781  .00012793  00000-0  47944-3 0  9998
2 62369  52.9976 203.5154 0008435 342.0440  18.0259 15.27596770 41754
Epoch: 2025-08-29T03:47Z
TLE epoch observation values (Epoch: 2025-08-29T03:47:47.426Z)
Latitude
0.00002°
Longitude
168.95695°
Altitude
478.377 km
Speed
7.631 km/s
True Right ascension
13h 34m 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
14:28:29
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
489.069 km
Perigee altitude
477.494 km
Semi-major axis
6,861.418 km
Eccentricity
0.00084
Inclination
52.9976°
RAAN
203.5154°
Arg. of periapsis
342.044°
True anomaly
18.05584°
Mean anomaly
18.0259°
Eccentric anomaly
18.04087°
Mean motion
3.81876 °/min
Orbital period
94.27 mins
BSTAR
0.00047944
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