CZ-7 R/B, 64787 (Decayed)
Orbit data source: Space-Track
CZ-7 R/B, 64787 was space debris in LEO originally from a launch on Mon, 14 Jul 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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64787 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-7 STAGE 2, Unknown motor
Mass
6,000 kg wet, 6,000 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: 1 month ago
TLE from 1 month ago
0 CZ-7 R/B
1 64787U 25149B 25210.12069650 .24558847 84300-5 12482-3 0 9995
2 64787 41.4489 118.9760 0017956 276.2662 187.5175 16.54061891 2305Epoch: 2025-07-29T02:53Z
TLE epoch observation values (Epoch: 2025-07-29T02:53:48.177Z)
Latitude
40.17354°
Longitude
-123.38622°
Altitude
142.48 km
Speed
7.82 km/s
True Right ascension
15h 08m 20s
True Declination
39° 59' 17"
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
11:28:48
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
142.673 km
Perigee altitude
119.298 km
Semi-major axis
6,509.123 km
Eccentricity
0.0018
Inclination
41.4489°
RAAN
118.976°
Arg. of periapsis
276.2662°
True anomaly
187.49064°
Mean anomaly
187.5175°
Eccentric anomaly
187.50406°
Mean motion
4.13294 °/min
Orbital period
87.1 mins
BSTAR
0.00012482
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Other satellites on launch #149 in the year 2025 (2025-07-14 UTC)
CZ-7 R/B Visibility
Observer location: undefined°, undefined°
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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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