CZ-2F DEB, 67692 (Decayed)
Orbit data source: Space-Track
CZ-2F DEB, 67692 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.
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67692 intel report (Beta)
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Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
CALT?
Mission
Decayed spacecraft
Bus & Motor
Unknown
Mass
1 kg wet, 1 kg dry
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Cone, 1.1 m
Radar Cross Section
0.025 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 2 weeks ago
TLE from 2 weeks ago
0 CZ-2F DEB
1 67692U 26024D 26142.85013849 .18242918 11998-4 23470-2 0 9992
2 67692 50.2906 357.6572 0024272 250.0072 109.8319 16.33850894 16164Epoch: 2026-05-22T20:24Z
TLE epoch observation values (Epoch: 2026-05-22T20:24:11.965Z)
Latitude
-0.00002°
Longitude
171.13226°
Altitude
188.261 km
Speed
7.792 km/s
True Right ascension
23h 50m 37s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
12:28:45
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
198.894 km
Perigee altitude
167.044 km
Semi-major axis
6,561.106 km
Eccentricity
0.00243
Inclination
50.2906°
RAAN
357.6572°
Arg. of periapsis
250.0072°
True anomaly
110.09327°
Mean anomaly
109.8319°
Eccentric anomaly
109.96261°
Mean motion
4.08392 °/min
Orbital period
88.15 mins
BSTAR
0.002347
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Other satellites on launch #24 in the year 2026 (2026-02-07 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.CZ-2F DEB Visibility
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
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| This satellite is decayed. |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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