DECAYED

CZ-2F DEB, 67718 (Decayed)

Orbit data source: Space-Track

CZ-2F DEB, 67718 was space debris in LEO originally from a launch on Sat, 07 Feb 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.

Not visible in the next 10 days
Identifier
67718, 2026-024E
Orbit
Decayed
Country
Flag of CNCN / PRC
Related business
Manufacturer
CALT?
Mission
Decayed spacecraft
Bus & Motor
Unknown
Mass
1 kg wet, 1 kg dry
Launch date (UTC)
2026-02-07 (4 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: 4 weeks ago

TLE from 4 weeks ago
0 CZ-2F DEB
1 67718U 26024E   26133.00369634  .00811346  24541-3  31629-2 0  9994
2 67718  50.3003  51.2048 0089364 190.9751 168.9284 15.80251713 14606
Epoch: 2026-05-13T00:05Z
TLE epoch observation values (Epoch: 2026-05-13T00:05:19.363Z)
Latitude
-0.00005°
Longitude
179.10413°
Altitude
389.174 km
Speed
7.644 km/s
True Right ascension
03h 24m 49s
True Declination
0° 00' 00"
Sunlit
Object was in daylight 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
12:30:19
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
390.419 km
Perigee altitude
270.517 km
Semi-major axis
6,708.605 km
Eccentricity
0.00894
Inclination
50.3003°
RAAN
51.2048°
Arg. of periapsis
190.9751°
True anomaly
169.12292°
Mean anomaly
168.9284°
Eccentric anomaly
169.02587°
Mean motion
3.94998 °/min
Orbital period
91.14 mins
BSTAR
0.0031629
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