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 (5 months ago)
Launch vehicle
Unknown
Launch site
Jiuquan Satellite Launch Center, China (JSC)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl, 3.1 m
Radar Cross Section
23.715 m², Large (>1 m²)

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   26170.88497950  .00001810  00000-0  12191-3 0  9999
2 67475  97.1581 233.8962 0098528  50.3951 310.5924 15.03940834 23433
Epoch: 2026-06-19T21:14Z
TLE epoch observation values (Epoch: 2026-06-19T21:14:22.228Z)
Latitude
0.00004°
Longitude
7.19604°
Altitude
513.77 km
Speed
7.631 km/s
True Right ascension
15h 35m 35s
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
10:18:36
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
620.014 km
Perigee altitude
483.457 km
Semi-major axis
6,929.872 km
Eccentricity
0.00985
Inclination
97.1581°
RAAN
233.8962°
Arg. of periapsis
50.3951°
True anomaly
309.72816°
Mean anomaly
310.5924°
Eccentric anomaly
310.16097°
Mean motion
3.76232 °/min
Orbital period
95.69 mins
BSTAR
0.00012191
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Other satellites on launch #9 in the year 2026 (2026-01-15 UTC)

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