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
Identifier
60751, 2024-153G
Orbit
Decayed
Last TLE update
5 months ago
Origin
Manufacturer
Xinghe Dongli
Mission
Decayed spacecraft
Bus & Motor
EDGE, EDGE
Mass
150 kg wet, ~150 kg dry
Launch date (UTC)
2024-08-29 (8 months ago)
Launch vehicle
Unknown
Launch site
Yellow Sea Launch Area, China (YSLA)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl, 1.2 m
Radar Cross Section
1.602 m², Large (>1 m²)

Expand to show TLE details & history

TLE from 5 months 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
Visualization observer readout
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
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CERES-1 R/B Visibility forecast

Observer location: undefined°, undefined°

This satellite is decayed
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