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 (4 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   26097.50675757  .00098956 -25770-6  12541-2 0  9995
2 66991  28.0897 249.4274 6849224 265.8430  19.9041  2.90618613  3128
Epoch: 2026-04-07T12:09Z
TLE epoch observation values (Epoch: 2026-04-07T12:09:43.854Z)
Latitude
-0°
Longitude
-128.87061°
Altitude
5,196.563 km
Speed
7.047 km/s
True Right ascension
16h 37m 22s
True Declination
0° 00' 00"
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
20:49:47
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
28,576.901 km
Perigee altitude
158.395 km
Semi-major axis
20,745.785 km
Eccentricity
0.68492
Inclination
28.0897°
RAAN
249.4274°
Arg. of periapsis
265.843°
True anomaly
94.23816°
Mean anomaly
19.9041°
Eccentric anomaly
49.93942°
Mean motion
0.72635 °/min
Orbital period
495.63 mins
BSTAR
0.0012541
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Other satellites on launch #290 in the year 2025 (2025-12-09 UTC)

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