CZ-4B R/B, 25732

Orbit data source: Space-Track

CZ-4B R/B, 25732 is space debris in SSO originally from a launch on Mon, 10 May 1999 UTC launched from the Taiyaun Space Center, China (TSC). 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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Identifier
25732, 1999-025C
Orbit
SSO
Country
Flag of CNCN / PRC
Related business
Manufacturer
SAST
Mission
Spacecraft
Bus & Motor
CZ-4 STAGE 3, Unknown motor
Mass
~1,000 kg wet, ~1,000 kg dry
Launch date (UTC)
1999-05-10 (27 years ago)
Launch vehicle
Unknown
Launch site
Taiyaun Space Center, China (TSC)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown
Radar Cross Section
Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 12 hours ago

TLE from 12 hours ago
0 CZ-4B R/B
1 25732U 99025C   25362.97637991  .00000096  00000-0  66959-4 0  9997
2 25732  98.6747  43.8915 0037034 186.7610 238.6325 14.18247745378143
Epoch: 2025-12-28T23:25Z
TLE epoch observation values (Epoch: 2025-12-28T23:25:59.224Z)
Latitude
63.75033°
Longitude
-63.20984°
Altitude
856.197 km
Speed
7.423 km/s
True Right ascension
01h 43m 52s
True Declination
63° 36' 56"
Sunlit
Object was in full shadow at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
10:32:32
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
855.133 km
Perigee altitude
801.755 km
Semi-major axis
7,206.581 km
Eccentricity
0.0037
Inclination
98.6747°
RAAN
43.8915°
Arg. of periapsis
186.761°
True anomaly
238.27102°
Mean anomaly
238.6325°
Eccentric anomaly
238.45167°
Mean motion
3.54772 °/min
Orbital period
101.47 mins
BSTAR
0.000066959
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