DECAYED

OBJECT H, 61234 (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, 61234 was a Chinese satellite in LEO that was launched on Tue, 24 Sep 2024 UTC via a JIELONG-3 launch vehicle from the Yellow Sea Launch Area, China (YSLA). 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
61234, 2024-173H
Orbit
Decayed
Country
Flag of CNCN / PRC
Related business
None
Manufacturer
ZZQY
Mission
Decayed Commercial Imaging
Bus & Motor
Unknown
Mass
~70 kg wet, ~70 kg dry
Launch date (UTC)
2024-09-24 (11 months ago)
Launch vehicle
JIELONG-3
Launch site
Yellow Sea Launch Area, China (YSLA)
Object type
Unknown
Shape & HBR
Box + 2 Pan, 0.3 m
Radar Cross Section
0.120 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 3 months ago

TLE from 3 months ago
0 OBJECT H
1 61234U 24173H   25157.21608585  .09436605  24643-5  19619-2 0  9993
2 61234  97.3455 241.6879 0013879 264.2704  95.7008 16.30791218 39415
Epoch: 2025-06-06T05:11Z
TLE epoch observation values (Epoch: 2025-06-06T05:11:09.817Z)
Latitude
-0.00005°
Longitude
-90.97654°
Altitude
194.573 km
Speed
7.789 km/s
True Right ascension
16h 06m 45s
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
02:57:58
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
196.344 km
Perigee altitude
178.119 km
Semi-major axis
6,565.368 km
Eccentricity
0.00139
Inclination
97.3455°
RAAN
241.6879°
Arg. of periapsis
264.2704°
True anomaly
95.85903°
Mean anomaly
95.7008°
Eccentric anomaly
95.77992°
Mean motion
4.07995 °/min
Orbital period
88.24 mins
BSTAR
0.0019619
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