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: 1 day ago

TLE from 1 day ago
0 SPACEMOBILE-SSR03 DEB
1 62371U 24163H   26259.22811875  .00023765  00000-0  52512-3 0  9994
2 62371  52.9690 198.8696 0009458  86.3336 273.8750 15.43710677105935
Epoch: 2026-09-16T05:28Z
TLE epoch observation values (Epoch: 2026-09-16T05:28:29.460Z)
Latitude
-0.00001°
Longitude
121.56412°
Altitude
435.624 km
Speed
7.652 km/s
True Right ascension
13h 15m 28s
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
02:59:35
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
441.902 km
Perigee altitude
429.014 km
Semi-major axis
6,813.595 km
Eccentricity
0.00095
Inclination
52.969°
RAAN
198.8696°
Arg. of periapsis
86.3336°
True anomaly
273.76686°
Mean anomaly
273.875°
Eccentric anomaly
273.82093°
Mean motion
3.85903 °/min
Orbital period
93.29 mins
BSTAR
0.00052512
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