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 (10 months ago)
Launch vehicle
Unknown
Launch site
Xichang Space Center, China (XSC)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl + 1 Nozzle, 6.4 m
Radar Cross Section
32.704 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 7 hours ago

TLE from 7 hours ago
0 CZ-3B R/B
1 66991U 25290B   26285.97307873  .00240147  30179-6  27336-2 0  9993
2 66991  28.0110 151.7772 6712187  65.6489 348.4817  3.09790091  8736
Epoch: 2026-10-12T23:21Z
TLE epoch observation values (Epoch: 2026-10-12T23:21:14.002Z)
Latitude
0.00007°
Longitude
140.00041°
Altitude
2,150.749 km
Speed
8.568 km/s
True Right ascension
10h 07m 24s
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
00:23:31
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
26,847.24 km
Perigee altitude
158.34 km
Semi-major axis
19,880.927 km
Eccentricity
0.67122
Inclination
28.011°
RAAN
151.7772°
Arg. of periapsis
65.6489°
True anomaly
294.64485°
Mean anomaly
348.4817°
Eccentric anomaly
328.23734°
Mean motion
0.77426 °/min
Orbital period
464.96 mins
BSTAR
0.0027336
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Other satellites on launch #290 in the year 2025 (2025-12-09 UTC)

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