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.
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63633 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CN / PRCRelated business
None
Manufacturer
CALT?
Mission
Decayed spacecraft
Bus & Motor
CZ-2F, Unknown motor
Mass
5,500 kg wet, 5,500 kg dry
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Unknown
Radar Cross Section
Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 5 months ago
TLE from 5 months 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 1314Epoch: 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
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
03:39:16
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
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
246.96504°
Mean anomaly
247.2406°
Eccentric anomaly
247.10278°
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)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.CZ-2F R/B Visibility
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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. |
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| This satellite is decayed. |
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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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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