CZ-2C DEB, 67587

Orbit data source: Space-Track

CZ-2C DEB, 67587 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
67587, 2026-009D
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, 0.1 m
Radar Cross Section
0.025 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 9 hours ago

TLE from 9 hours ago
0 CZ-2C DEB
1 67587U 26009D   26171.47956769  .00048096  00000-0  15587-2 0  9995
2 67587  97.6561 248.5773 0078207  44.7914 315.9603 15.28864574 23730
Epoch: 2026-06-20T11:30Z
TLE epoch observation values (Epoch: 2026-06-20T11:30:34.648Z)
Latitude
-0.00003°
Longitude
167.23934°
Altitude
443.945 km
Speed
7.667 km/s
True Right ascension
16h 34m 18s
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
07:24:11
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
529.775 km
Perigee altitude
422.564 km
Semi-major axis
6,854.307 km
Eccentricity
0.00782
Inclination
97.6561°
RAAN
248.5773°
Arg. of periapsis
44.7914°
True anomaly
315.33291°
Mean anomaly
315.9603°
Eccentric anomaly
315.64705°
Mean motion
3.8247 °/min
Orbital period
94.12 mins
BSTAR
0.0015587
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Other satellites on launch #9 in the year 2026 (2026-01-15 UTC)

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