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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67690 intel report (Beta)
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Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
CALT?
Mission
Spacecraft
Bus & Motor
CZ-2F, Unknown motor
Mass
5,500 kg wet, 5,500 kg dry
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Unknown shape, 8.0 m
Radar Cross Section
RCS unknown
Expand to show TLE details & historyLast TLE update: 13 hours ago
TLE from 13 hours ago
0 CZ-2F R/B
1 67690U 26024B 26103.98636886 .00010209 00000-0 18683-3 0 9999
2 67690 49.9861 197.3769 0170163 61.4437 300.3532 15.35644866 10119Epoch: 2026-04-13T23:40Z
TLE epoch observation values (Epoch: 2026-04-13T23:40:22.269Z)
Latitude
-0.00006°
Longitude
0.11496°
Altitude
402.265 km
Speed
7.703 km/s
True Right ascension
13h 09m 30s
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
19:33:39
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
576.14 km
Perigee altitude
343.428 km
Semi-major axis
6,837.921 km
Eccentricity
0.01702
Inclination
49.9861°
RAAN
197.3769°
Arg. of periapsis
61.4437°
True anomaly
298.65253°
Mean anomaly
300.3532°
Eccentric anomaly
299.50468°
Mean motion
3.83846 °/min
Orbital period
93.79 mins
BSTAR
0.00018683
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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 R/B Visibility forecast
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-04-14 14:09:15.755Z | 328.664° NNW | 2026-04-14 14:11:15.755Z | 13.6° NNE | 21.089° | 2026-04-14 14:13:15.755Z | 66.475° ENE |
| 4 mins | 2026-04-14 15:48:15.755Z | 278.852° WNW | 2026-04-14 15:49:15.755Z | 231.478° WSW | 38.663° | 2026-04-14 15:52:15.755Z | 141.542° SSE |
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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Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in descending order |
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