CZ-2F R/B, 67690
Orbit data source: Space-Track
CZ-2F R/B, 67690 is space debris in LEO originally from a Chinese 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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Edit Public Description
Identifier
Orbit
Country
CN / PRCRelated business
None
Manufacturer
Unknown
Mission
Spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Unknown
Radar Cross Section
RCS unknown
Expand to show TLE details & historyLast TLE update: 6 hours ago
TLE from 6 hours ago
0 CZ-2F R/B
1 67690U 26024B 26039.64517463 .00010042 00000-0 19429-3 0 9993
2 67690 49.9868 160.1378 0178096 154.4940 206.4941 15.33016351 237Epoch: 2026-02-08T15:29Z
TLE epoch observation values (Epoch: 2026-02-08T15:29:03.088Z)
Latitude
0.00005°
Longitude
149.1236°
Altitude
576.894 km
Speed
7.513 km/s
True Right ascension
10h 40m 33s
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
23:57:39
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
589.516 km
Perigee altitude
345.676 km
Semi-major axis
6,845.733 km
Eccentricity
0.01781
Inclination
49.9868°
RAAN
160.1378°
Arg. of periapsis
154.494°
True anomaly
205.60151°
Mean anomaly
206.4941°
Eccentric anomaly
206.04604°
Mean motion
3.83189 °/min
Orbital period
93.95 mins
BSTAR
0.00019429
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-02-09 10:26:06.381Z | 208.452° SW | 2026-02-09 10:29:06.381Z | 135.922° SSE | 35.11° | 2026-02-09 10:32:06.381Z | 69.438° E |
| 5 mins | 2026-02-09 12:05:06.381Z | 283.634° WNW | 2026-02-09 12:07:06.381Z | 335.618° NNW | 28.154° | 2026-02-09 12:10:06.381Z | 39.827° NE |
| 4 mins | 2026-02-09 17:01:06.381Z | 304.12° NW | 2026-02-09 17:03:06.381Z | 132.314° SE | 44.818° | 2026-02-09 17:05:06.381Z | 125.458° SE |
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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