CZ-2F R/B, 67690

Orbit data source: Space-Track

CZ-2F R/B, 67690 is 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.

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Identifier
67690, 2026-024B
Orbit
LEO
Country
Flag of CNCN / PRC
Related business
Manufacturer
CALT?
Mission
Spacecraft
Bus & Motor
CZ-2F, Unknown motor
Mass
5,500 kg wet, 5,500 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
Cyl, 3.8 m
Radar Cross Section
44.450 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 4 days ago

TLE from 4 days ago
0 CZ-2F R/B
1 67690U 26024B   26154.58876600  .00014025  00000-0  24411-3 0  9997
2 67690  49.9877 302.8080 0166985 272.7881  85.3978 15.36998294 17896
Epoch: 2026-06-03T14:07Z
TLE epoch observation values (Epoch: 2026-06-03T14:07:49.382Z)
Latitude
-0.00005°
Longitude
-161.19302°
Altitude
448.289 km
Speed
7.649 km/s
True Right ascension
20h 11m 13s
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
12:28:47
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
569.886 km
Perigee altitude
341.654 km
Semi-major axis
6,833.907 km
Eccentricity
0.0167
Inclination
49.9877°
RAAN
302.808°
Arg. of periapsis
272.7881°
True anomaly
87.30798°
Mean anomaly
85.3978°
Eccentric anomaly
86.35262°
Mean motion
3.84184 °/min
Orbital period
93.71 mins
BSTAR
0.00024411
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