CZ-2C R/B, 67475

Orbit data source: Space-Track

CZ-2C R/B, 67475 is space debris in SSO originally from a launch on Thu, 15 Jan 2026 UTC launched from the Jiuquan Satellite Launch Center, China (JSC). 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
67475, 2026-009B
Orbit
SSO
Country
Flag of CNCN / PRC
Related business
Manufacturer
CALT
Mission
Spacecraft
Bus & Motor
CZ-2 STAGE 2, Unknown motor
Mass
~3,800 kg wet, ~3,800 kg dry
Launch date (UTC)
2026-01-15 (2 months ago)
Launch vehicle
Unknown
Launch site
Jiuquan Satellite Launch Center, China (JSC)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown shape, 8.0 m
Radar Cross Section
RCS unknown

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

TLE from 1 day ago
0 CZ-2C R/B
1 67475U 26009B   26065.20676429  .00004743  00000-0  31788-3 0  9999
2 67475  97.1688 136.0135 0099060  52.4821 308.5358 15.03312180  7558
Epoch: 2026-03-06T04:57Z
TLE epoch observation values (Epoch: 2026-03-06T04:57:44.434Z)
Latitude
-0.00005°
Longitude
-102.36772°
Altitude
517.379 km
Speed
7.628 km/s
True Right ascension
09h 04m 03s
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
08:35:31
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
622.336 km
Perigee altitude
485.003 km
Semi-major axis
6,931.806 km
Eccentricity
0.00991
Inclination
97.1688°
RAAN
136.0135°
Arg. of periapsis
52.4821°
True anomaly
307.641°
Mean anomaly
308.5358°
Eccentric anomaly
308.08909°
Mean motion
3.76074 °/min
Orbital period
95.73 mins
BSTAR
0.00031788
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Other satellites on launch #9 in the year 2026 (2026-01-15 UTC)

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