DECAYED

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.

Not visible in the next 10 days
CZ-2C R/B details
Identifier
60090, 2024-116C
Orbit
Decayed
Last TLE update5 months ago
Origin
Flag of CNCASC (CN / PRC)
ManufacturerCALT
MissionDecayed spacecraft
Bus & MotorCZ-2 STAGE 2, Unknown motor
Mass~3,800 kg wet, ~3,800 kg dry
Launch date (UTC)
2024-06-22 (7 months ago)
Launch vehicleUnknown
Launch site
Xichang Space Center, China (XSC)
Object type
Payload
Rocket body
Debris
Shape & HBRCyl, 7.49 m
Radar Cross Section23.715 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)
Latitude17.56557°
Longitude166.07812°
Altitude159.526 km
Speed7.807 km/s
True Right ascension05h 28m 59s
True Declination17° 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 altitude168.956 km
Perigee altitude136.476 km
Semi-major axis6,530.853 km
Eccentricity0.0024867
Inclination27.9996°
RAAN45.9526°
Arg. of periapsis188.3258°
True anomaly211.46851°
Mean anomaly211.6175°
Eccentric anomaly211.54296°
Mean motion4.11233 °/min
BSTAR0.00042652
Orbital period87.54 mins
Loading maneuver chart data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Other satellites on launch #116 in the year 2024 (2024-06-22 UTC)

CZ-2C R/B Visibility forecast

Observer location: undefined°, undefined

This satellite is decayed
Span
Click to sort rows by Start time (UTC) header in descending order
Start Az.
Max El. time (UTC)
Max El. Az.
Max El.
End time (UTC)
End Az.
|