OBJECT A, 67689
Orbit data source: Space-Track
You're viewing an Uncataloged Satellite
Recently launched and/or uncataloged satellites may have evolving metadata. Metadata may include but not limited to: Owner, Maufacturer, Bus, Motor, and Mission.
OBJECT A, 67689 is a Chinese satellite in LEO that was launched on Sat, 07 Feb 2026 UTC launched from the Jiuquan Satellite Launch Center, China (JSC). Unknown objects in Earth's orbit typically refer to objects detected orbiting the Earth but have not yet been identified or cataloged. These objects could be anything from previously untracked satellites, spent rocket stages, debris from satellite collisions, or even natural meteoroids temporarily captured by Earth's gravity.
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67689 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CN / PRCRelated business
None
Manufacturer
Unknown
Mission
Operational spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Unknown
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 OBJECT A
1 67689U 26024A 26039.64547411 .00009277 00000-0 18096-3 0 9994
2 67689 49.9899 160.1377 0179624 154.5769 206.4162 15.32684951 237Epoch: 2026-02-08T15:29Z
TLE epoch observation values (Epoch: 2026-02-08T15:29:28.963Z)
Latitude
0.00003°
Longitude
149.01538°
Altitude
578.912 km
Speed
7.511 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
23:57:34
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
591.566 km
Perigee altitude
345.599 km
Semi-major axis
6,846.719 km
Eccentricity
0.01796
Inclination
49.9899°
RAAN
160.1377°
Arg. of periapsis
154.5769°
True anomaly
205.51857°
Mean anomaly
206.4162°
Eccentric anomaly
205.9656°
Mean motion
3.83106 °/min
Orbital period
93.97 mins
BSTAR
0.00018096
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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.OBJECT A 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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-02-09 10:26:01.340Z | 212.977° SW | 2026-02-09 10:30:01.340Z | 125.311° SE | 34.989° | 2026-02-09 10:33:01.340Z | 68.033° E |
| 4 mins | 2026-02-09 12:06:01.340Z | 286.69° WNW | 2026-02-09 12:08:01.340Z | 342.291° N | 27.847° | 2026-02-09 12:10:01.340Z | 31.171° NE |
| 4 mins | 2026-02-09 17:02:01.340Z | 303.57° NW | 2026-02-09 17:04:01.340Z | 134.019° SE | 44.062° | 2026-02-09 17:06:01.340Z | 126.14° 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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