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: 10 hours ago

TLE from 10 hours ago
0 SPACEMOBILE-SSR05 DEB
1 62373U 24163K   26093.49722617  .00027135  00000-0  86275-3 0  9994
2 62373  52.9753 274.0089 0006668 267.2617  92.7619 15.32423750 86663
Epoch: 2026-04-03T11:56Z
TLE epoch observation values (Epoch: 2026-04-03T11:56:00.341Z)
Latitude
-0.00001°
Longitude
-96.82303°
Altitude
469.687 km
Speed
7.632 km/s
True Right ascension
18h 16m 02s
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
03:42:02
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
473.436 km
Perigee altitude
464.304 km
Semi-major axis
6,847.007 km
Eccentricity
0.00067
Inclination
52.9753°
RAAN
274.0089°
Arg. of periapsis
267.2617°
True anomaly
92.83822°
Mean anomaly
92.7619°
Eccentric anomaly
92.80006°
Mean motion
3.83082 °/min
Orbital period
93.97 mins
BSTAR
0.00086275
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