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 (1 month ago)
Launch vehicle
Unknown
Launch site
Jiuquan Satellite Launch Center, China (JSC)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown
Radar Cross Section
RCS unknown

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

TLE from 9 hours ago
0 CZ-2F R/B
1 67690U 26024B   26071.95911763  .00018019  00000-0  32936-3 0  9994
2 67690  49.9887 358.1993 0173925 288.4028  69.8090 15.34471678  5195
Epoch: 2026-03-12T23:01Z
TLE epoch observation values (Epoch: 2026-03-12T23:01:07.763Z)
Latitude
-0.00001°
Longitude
-157.68458°
Altitude
423.823 km
Speed
7.68 km/s
True Right ascension
23h 52m 47s
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
12:31:21
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
582.257 km
Perigee altitude
344.279 km
Semi-major axis
6,841.405 km
Eccentricity
0.01739
Inclination
49.9887°
RAAN
358.1993°
Arg. of periapsis
288.4028°
True anomaly
71.69335°
Mean anomaly
69.809°
Eccentric anomaly
70.7498°
Mean motion
3.83553 °/min
Orbital period
93.86 mins
BSTAR
0.00032936
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