CZ-7A R/B, 63398 (Decayed)
Orbit data source: Space-Track
CZ-7A R/B, 63398 was space debris in LEO originally from a launch on Sat, 29 Mar 2025 UTC launched from the Wenchang Satellite Launch Center (WSC). 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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63398 intel report (Beta)
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Edit Public Description
Expand to show TLE details & historyLast TLE update: 1 month ago
TLE from 1 month ago
0 CZ-7A R/B
1 63398U 25064B 25208.88579138 .99999999 -26849-4 36009-2 0 9998
2 63398 19.6756 358.6821 1647909 345.4543 113.2533 12.70228566 3877
Epoch: 2025-07-27T21:15Z
TLE epoch observation values (Epoch: 2025-07-27T21:15:32.375Z)
Latitude
17.90746°
Longitude
-150.11418°
Altitude
2,042.627 km
Speed
6.584 km/s
True Right ascension
07h 38m 17s
True Declination
17° 49' 21"
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
18:01:16
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
2,665.372 km
Perigee altitude
106.479 km
Semi-major axis
7,764.063 km
Eccentricity
0.16479
Inclination
19.6756°
RAAN
358.6821°
Arg. of periapsis
345.4543°
True anomaly
129.09311°
Mean anomaly
113.2533°
Eccentric anomaly
121.3193°
Mean motion
3.17256 °/min
Orbital period
113.47 mins
BSTAR
0.0036009
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Other satellites on launch #64 in the year 2025 (2025-03-29 UTC)
CZ-7A R/B Visibility
Observer location: undefined°, undefined°
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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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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Authenticating...
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