CZ-3B R/B, 66991

Orbit data source: Space-Track

CZ-3B R/B, 66991 is space debris in HEO originally from a launch on Tue, 09 Dec 2025 UTC launched from the Xichang Space Center, China (XSC). 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
66991, 2025-290B
Orbit
HEO
Country
Flag of CNCN / PRC
Related business
Manufacturer
CALT
Mission
Spacecraft
Bus & Motor
CZ-3A STAGE 3, Unknown motor
Mass
~2,800 kg wet, ~2,800 kg dry
Launch date (UTC)
2025-12-09 (6 months ago)
Launch vehicle
Unknown
Launch site
Xichang Space Center, China (XSC)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl + 1 Nozzle, 8.0 m
Radar Cross Section
32.704 m²

Expand to show TLE details & history
Last TLE update: 1 day ago

TLE from 1 day ago
0 CZ-3B R/B
1 66991U 25290B   26145.23785059  .00019798  89534-6  77892-3 0  9991
2 66991  28.0667 225.0258 6803930 305.6697   8.7240  2.94876464  4523
Epoch: 2026-05-25T05:42Z
TLE epoch observation values (Epoch: 2026-05-25T05:42:30.290Z)
Latitude
-0.00012°
Longitude
-103.42754°
Altitude
1,531.106 km
Speed
9.021 km/s
True Right ascension
15h 00m 06s
True Declination
0° 00' 00"
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
19:52:27
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
28,146.556 km
Perigee altitude
188.383 km
Semi-major axis
20,545.606 km
Eccentricity
0.68039
Inclination
28.0667°
RAAN
225.0258°
Arg. of periapsis
305.6697°
True anomaly
54.87853°
Mean anomaly
8.724°
Eccentric anomaly
25.51786°
Mean motion
0.737 °/min
Orbital period
488.47 mins
BSTAR
0.00077892
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Other satellites on launch #290 in the year 2025 (2025-12-09 UTC)

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