DECAYED

CZ-2C R/B, 61620 (Decayed)

Orbit data source: Space-Track

CZ-2C R/B, 61620 was space debris in LEO originally from a launch on Wed, 23 Oct 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
Identifier
61620, 2024-190D
Orbit
Decayed
Last TLE update
6 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)
2024-10-23 (7 months ago)
Launch vehicle
Unknown
Launch site
Xichang Space Center, China (XSC)
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 6 months ago
0 CZ-2C R/B
1 61620U 24190D   24325.87196646  .05332485  15058-5  50849-3 0  9997
2 61620  34.9970 184.6356 0040246 310.7409 119.6211 16.34319024  4516
Epoch: 2024-11-20T20:55Z
TLE epoch observation values (Epoch: 2024-11-20T20:55:37.902Z)
Latitude
32.9322°
Longitude
-122.73039°
Altitude
194.193 km
Speed
7.788 km/s
True Right ascension
16h 46m 09s
True Declination
32° 45' 43"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Visualization observer readout
Orbital elements
Apogee altitude
210.777 km
Perigee altitude
157.954 km
Semi-major axis
6,562.502 km
Eccentricity
0.00402
Inclination
34.997°
RAAN
184.6356°
Arg. of periapsis
310.7409°
True anomaly
Unknown
Mean anomaly
119.6211°
Eccentric anomaly
Unknown
Mean motion
4.08262 °/min
Orbital period
88.18 mins
BSTAR
0.00050849
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Other satellites on launch #190 in the year 2024 (2024-10-23 UTC)

CZ-2C R/B Visibility

Observer location: undefined°, undefined°

This satellite is decayed
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