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
Cyl, 2.5 m
Radar Cross Section
14.536 m², 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   26124.11604277  .00000045  00000-0  42307-4 0  9996
2 25732  98.6522 167.0554 0037076 183.7244 236.1440 14.18275735396026
Epoch: 2026-05-04T02:47Z
TLE epoch observation values (Epoch: 2026-05-04T02:47:06.095Z)
Latitude
58.52418°
Longitude
-111.04413°
Altitude
856.007 km
Speed
7.422 km/s
True Right ascension
10h 10m 57s
True Declination
58° 22' 22"
Sunlit
Object was in daylight 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
22:40:32
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
855.067 km
Perigee altitude
801.629 km
Semi-major axis
7,206.485 km
Eccentricity
0.00371
Inclination
98.6522°
RAAN
167.0554°
Arg. of periapsis
183.7244°
True anomaly
235.79209°
Mean anomaly
236.144°
Eccentric anomaly
235.96795°
Mean motion
3.54779 °/min
Orbital period
101.47 mins
BSTAR
0.000042307
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