DECAYED

CERES-1 R/B, 60751 (Decayed)

Orbit data source: Space-Track

CERES-1 R/B, 60751 was space debris in LEO originally from a launch on Thu, 29 Aug 2024 UTC launched from the Yellow Sea Launch Area, China (YSLA). 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.

Not visible in the next 10 days

CERES-1 R/B details

Identifier	60751, 2024-153G
Orbit	Decayed
Last TLE update	3 weeks ago
Origin	Xinghe Dongli (CN / PRC)
Manufacturer	Xinghe Dongli
Mission	Decayed spacecraft
Bus & Motor	EDGE, EDGE
Mass	150 kg wet, ~150 kg dry
Launch date (UTC)	2024-08-29 (5 months ago)
Launch vehicle	Unknown
Launch site	Yellow Sea Launch Area, China (YSLA)
Object type	Payload Rocket body Debris
Shape & HBR	Unknown
Radar Cross Section	Large (>1 m²)

Expand to show TLE details & history

TLE from 3 weeks ago

0 CERES-1 R/B
1 60751U 24153G   24358.01649696  .15937085  27715-5  21901-3 0  9998
2 60751  97.6177 126.6125 0020523 285.1284 187.3470 16.47527681 18199

Epoch: 2024-12-23T00:23Z

Definitive object data (Epoch: 2024-12-23T00:23:45.337Z)

Latitude	66.45429°
Longitude	-133.60401°
Altitude	170.662 km
Speed	7.802 km/s
True Right ascension	21h 37m 31s
True Declination	66° 19' 00"
Sunlit	Object was in daylight at TLE epoch

Visualization observer readout

Observer readout values are unavailable because the object's trajectory could not be propagated. This is usually caused when the trajectory data is faulty or the object's orbit has decayed.

Visualization observer readout

Observer readout values are unavailable because the object's trajectory could not be propagated. This is usually caused when the trajectory data is faulty or the object's orbit has decayed.

Orbital elements

Apogee altitude	156.045 km
Perigee altitude	129.279 km
Semi-major axis	6,520.799 km
Eccentricity	0.0020523
Inclination	97.6177°
RAAN	126.6125°
Arg. of periapsis	285.1284°
True anomaly	187.317°
Mean anomaly	187.347°
Eccentric anomaly	187.33199°
Mean motion	4.12185 °/min
BSTAR	0.00021901
Orbital period	87.34 mins