CZ-2C DEB, 67586

Orbit data source: Space-Track

CZ-2C DEB, 67586 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
67586, 2026-009C
Orbit
SSO
Country
Flag of CNCN / PRC
Related business
Manufacturer
CALT?
Mission
Spacecraft
Bus & Motor
Unknown
Mass
1 kg wet, 1 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, 1.1 m
Radar Cross Section
RCS unknown

Expand to show TLE details & history
Last TLE update: 10 hours ago

TLE from 10 hours ago
0 CZ-2C DEB
1 67586U 26009C   26065.76886718  .00058739  00000-0  27049-2 0  9995
2 67586  97.2201 137.9143 0102670  47.1329 313.8470 15.15424291  7642
Epoch: 2026-03-06T18:27Z
TLE epoch observation values (Epoch: 2026-03-06T18:27:10.124Z)
Latitude
-0.00001°
Longitude
56.622°
Altitude
474.092 km
Speed
7.656 km/s
True Right ascension
09h 11m 39s
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
08:34:14
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
587.443 km
Perigee altitude
445.866 km
Semi-major axis
6,894.791 km
Eccentricity
0.01027
Inclination
97.2201°
RAAN
137.9143°
Arg. of periapsis
47.1329°
True anomaly
312.99093°
Mean anomaly
313.847°
Eccentric anomaly
313.41973°
Mean motion
3.79107 °/min
Orbital period
94.96 mins
BSTAR
0.0027049
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Other satellites on launch #9 in the year 2026 (2026-01-15 UTC)

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