DECAYED

CZ-2F R/B, 63633 (Decayed)

Orbit data source: Space-Track

CZ-2F R/B, 63633 was space debris in LEO originally from a launch on Thu, 24 Apr 2025 UTC launched from the Jiuquan Satellite Launch Center, China (JSC). 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
63633, 2025-082B
Orbit
Decayed
Last TLE update
3 weeks ago
Origin
Unknown
Manufacturer
Unknown
Mission
Decayed spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
2025-04-24 (4 weeks ago)
Launch vehicle
Unknown
Launch site
Jiuquan Satellite Launch Center, China (JSC)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown
Radar Cross Section
Large (>1 m²)

Expand to show TLE details & history

TLE from 3 weeks ago
0 CZ-2F R/B
1 63633U 25082B   25122.79872868  .12669141  78614-5  34580-3 0  9999
2 63633  41.4570 292.5240 0026111 206.6050 247.2406 16.42622166  1314
Epoch: 2025-05-02T19:10Z
TLE epoch observation values (Epoch: 2025-05-02T19:10:10.157Z)
Latitude
41.52272°
Longitude
-121.20485°
Altitude
168.009 km
Speed
7.808 km/s
True Right ascension
01h 49m 09s
True Declination
41° 20' 12"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Visualization observer readout
Orbital elements
Apogee altitude
178.223 km
Perigee altitude
144.074 km
Semi-major axis
6,539.286 km
Eccentricity
0.00261
Inclination
41.457°
RAAN
292.524°
Arg. of periapsis
206.605°
True anomaly
Unknown
Mean anomaly
247.2406°
Eccentric anomaly
Unknown
Mean motion
4.10438 °/min
Orbital period
87.71 mins
BSTAR
0.0003458
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Other satellites on launch #82 in the year 2025 (2025-04-24 UTC)

CZ-2F R/B Visibility

Observer location: undefined°, undefined°

This satellite is decayed
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