SPACEMOBILE-SSR05 DEB, 62373

Orbit data source: Space-Track

SPACEMOBILE-SSR05 DEB, 62373 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
62373, 2024-163K
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-SSR05 DEB
1 62373U 24163K   26259.28489830  .00011545  00000-0  33786-3 0  9999
2 62373  52.9738 215.8722 0008997  78.0618 282.1391 15.35695841112116
Epoch: 2026-09-16T06:50Z
TLE epoch observation values (Epoch: 2026-09-16T06:50:15.213Z)
Latitude
Longitude
118.07012°
Altitude
458.448 km
Speed
7.64 km/s
True Right ascension
14h 23m 29s
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
02:59:36
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
465.293 km
Perigee altitude
452.99 km
Semi-major axis
6,837.279 km
Eccentricity
0.0009
Inclination
52.9738°
RAAN
215.8722°
Arg. of periapsis
78.0618°
True anomaly
282.03828°
Mean anomaly
282.1391°
Eccentric anomaly
282.08869°
Mean motion
3.839 °/min
Orbital period
93.77 mins
BSTAR
0.00033786
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