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.
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60751 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
Xinghe Dongli
Mission
Decayed spacecraft
Bus & Motor
EDGE, EDGE
Mass
150 kg wet, ~150 kg dry
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Cyl, 0.6 m
Radar Cross Section
1.602 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 8 months ago
TLE from 8 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 18199Epoch: 2024-12-23T00:23Z
TLE epoch observation values (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
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
15:36:35
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
156.045 km
Perigee altitude
129.279 km
Semi-major axis
6,520.799 km
Eccentricity
0.00205
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
Orbital period
87.34 mins
BSTAR
0.00021901
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Other satellites on launch #153 in the year 2024 (2024-08-29 UTC)
CERES-1 R/B Visibility
Observer location: undefined°, undefined°
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Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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Authenticating...
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