CZ-2C R/B, 60090 (Decayed)
Orbit data source: Space-Track
CZ-2C R/B, 60090 was space debris in LEO originally from a launch on Sat, 22 Jun 2024 UTC launched from the Xichang Space Center, China (XSC). 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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60090 intel report (Beta)
CZ-2C R/B details
Identifier | |
Orbit | Decayed |
Last TLE update | 5 months ago |
Origin | |
Manufacturer | CALT |
Mission | Decayed spacecraft |
Bus & Motor | CZ-2 STAGE 2, Unknown motor |
Mass | ~3,800 kg wet, ~3,800 kg dry |
Launch date (UTC) | |
Launch vehicle | Unknown |
Launch site | |
Object type | Payload Rocket body Debris |
Shape & HBR | Cyl, 7.49 m |
Radar Cross Section | 23.715 m², Large (>1 m²) |
Expand to show TLE details & history
TLE from 5 months ago
0 CZ-2C R/B
1 60090U 24116C 24217.89509560 .30682393 -88823-5 42652-3 0 9998
2 60090 27.9996 45.9526 0024867 188.3258 211.6175 16.46642363 6800
Epoch: 2024-08-04T21:28Z
Definitive object data (Epoch: 2024-08-04T21:28:56.259Z)
Latitude | 17.56557° |
Longitude | 166.07812° |
Altitude | 159.526 km |
Speed | 7.807 km/s |
True Right ascension | 05h 28m 59s |
True Declination | 17° 27' 28" |
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 | 168.956 km |
Perigee altitude | 136.476 km |
Semi-major axis | 6,530.853 km |
Eccentricity | 0.0024867 |
Inclination | 27.9996° |
RAAN | 45.9526° |
Arg. of periapsis | 188.3258° |
True anomaly | 211.46851° |
Mean anomaly | 211.6175° |
Eccentric anomaly | 211.54296° |
Mean motion | 4.11233 °/min |
BSTAR | 0.00042652 |
Orbital period | 87.54 mins |
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Other satellites on launch #116 in the year 2024 (2024-06-22 UTC)
OBJECT A, 60088 |
OBJECT B, 60089 |
CZ-2C R/B, 60090 (Decayed) |
CZ-2C R/B Visibility forecast
Observer location: undefined°, undefined
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