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 (5 months ago)
Launch vehicle
Unknown
Launch site
Jiuquan Satellite Launch Center, China (JSC)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cone, 1.1 m
Radar Cross Section
0.025 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 11 hours ago

TLE from 11 hours ago
0 CZ-2C DEB
1 67586U 26009C   26171.43062792  .00042482  00000-0  14718-2 0  9992
2 67586  97.2087 239.1363 0081384  36.1301 324.5399 15.26536117 23706
Epoch: 2026-06-20T10:20Z
TLE epoch observation values (Epoch: 2026-06-20T10:20:06.252Z)
Latitude
0.00005°
Longitude
175.46489°
Altitude
443.923 km
Speed
7.671 km/s
True Right ascension
15h 56m 32s
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
08:42:47
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
538.965 km
Perigee altitude
427.285 km
Semi-major axis
6,861.262 km
Eccentricity
0.00814
Inclination
97.2087°
RAAN
239.1363°
Arg. of periapsis
36.1301°
True anomaly
323.99436°
Mean anomaly
324.5399°
Eccentric anomaly
324.26758°
Mean motion
3.81889 °/min
Orbital period
94.27 mins
BSTAR
0.0014718
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Other satellites on launch #9 in the year 2026 (2026-01-15 UTC)

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