CZ-2F DEB, 67691 (Decayed)
Orbit data source: Space-Track
CZ-2F DEB, 67691 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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67691 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
Unknown shape, 1.1 m
Radar Cross Section
RCS unknown
Expand to show TLE details & historyLast TLE update: 1 month ago
TLE from 1 month ago
0 CZ-2F DEB
1 67691U 26024C 26069.88573476 .04187421 11818-4 73858-3 0 9998
2 67691 49.8977 356.8219 0080519 293.4265 65.8278 16.22770068 5014Epoch: 2026-03-10T21:15Z
TLE epoch observation values (Epoch: 2026-03-10T21:15:27.483Z)
Latitude
-0.00004°
Longitude
-130.60055°
Altitude
191.238 km
Speed
7.806 km/s
True Right ascension
23h 47m 17s
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
19:35:07
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
265.934 km
Perigee altitude
159.794 km
Semi-major axis
6,591.001 km
Eccentricity
0.00805
Inclination
49.8977°
RAAN
356.8219°
Arg. of periapsis
293.4265°
True anomaly
66.67303°
Mean anomaly
65.8278°
Eccentric anomaly
66.25007°
Mean motion
4.05617 °/min
Orbital period
88.75 mins
BSTAR
0.00073858
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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
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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