DECAYED

OBJECT H, 58924 (Decayed)

Orbit data source: Space-Track

You're viewing an Uncataloged Satellite

Recently launched and/or uncataloged satellites may have evolving metadata. Metadata may include but not limited to: Owner, Maufacturer, Bus, Motor, and Mission.

OBJECT H, 58924 was a satellite in LEO that was launched on Sat, 03 Feb 2024 UTC via a JIELONG-3 launch vehicle from the South China Sea Launch Area (SCSLA). Unknown objects in Earth's orbit typically refer to objects detected orbiting the Earth but have not yet been identified or cataloged. These objects could be anything from previously untracked satellites, spent rocket stages, debris from satellite collisions, or even natural meteoroids temporarily captured by Earth's gravity. This object's orbit decayed before it could be identified.

Not visible in the next 10 days
Identifier
58924, 2024-024H
Orbit
Decayed
Country
Flag of TBDTBD
Related business
None
Manufacturer
Unknown
Mission
Decayed Commercial Imaging
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
2024-02-03 (2 years ago)
Launch vehicle
JIELONG-3
Launch site
South China Sea Launch Area (SCSLA)
Object type
Unknown
Shape & HBR
Box, 0.2 m
Radar Cross Section
0.240 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 11 months ago

TLE from 11 months ago
0 OBJECT H
1 58924U 24024H   25198.81775610  .07929948  24785-5  90857-3 0  9991
2 58924  97.3151 287.9090 0014340 256.4964 103.4736 16.36601519118483
Epoch: 2025-07-17T19:37Z
TLE epoch observation values (Epoch: 2025-07-17T19:37:34.127Z)
Latitude
-0.00002°
Longitude
57.63869°
Altitude
180.311 km
Speed
7.797 km/s
True Right ascension
19h 11m 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
21:32:01
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
181.059 km
Perigee altitude
162.274 km
Semi-major axis
6,549.804 km
Eccentricity
0.00143
Inclination
97.3151°
RAAN
287.909°
Arg. of periapsis
256.4964°
True anomaly
103.63333°
Mean anomaly
103.4736°
Eccentric anomaly
103.55347°
Mean motion
4.0945 °/min
Orbital period
87.92 mins
BSTAR
0.00090857
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