OBJECT A, 67646
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, 67646 is a satellite owned by ASAL (CN) in SSO that was launched on Sat, 31 Jan 2026 UTC via a CHANG ZHENG 2C launch vehicle 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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67646 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
CAST
Mission
Operational spacecraft
Bus & Motor
CAST-2000?, Unknown motor
Mass
~500 kg wet, ~500 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Unknown
Shape & HBR
Unknown
Radar Cross Section
RCS unknown
Expand to show TLE details & historyLast TLE update: 10 hours ago
TLE from 10 hours ago
0 OBJECT A
1 67646U 26021A 26039.94723883 .00007234 00000-0 30550-3 0 9996
2 67646 97.4720 114.4068 0011595 232.3575 127.6611 15.23508168 1343Epoch: 2026-02-08T22:44Z
TLE epoch observation values (Epoch: 2026-02-08T22:44:01.434Z)
Latitude
0.00001°
Longitude
-5.64828°
Altitude
503.238 km
Speed
7.61 km/s
True Right ascension
07h 37m 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
11:24:32
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
500.199 km
Perigee altitude
484.267 km
Semi-major axis
6,870.37 km
Eccentricity
0.00116
Inclination
97.472°
RAAN
114.4068°
Arg. of periapsis
232.3575°
True anomaly
127.76619°
Mean anomaly
127.6611°
Eccentric anomaly
127.71365°
Mean motion
3.8113 °/min
Orbital period
94.46 mins
BSTAR
0.0003055
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Other satellites on launch #21 in the year 2026 (2026-01-31 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-02-09 18:13:07.123Z | 345.094° N | 2026-02-09 18:15:07.123Z | 295.84° NW | 30.424° | 2026-02-09 18:18:07.123Z | 223.477° SW |
| 6 mins | 2026-02-10 04:49:07.123Z | 160.576° S | 2026-02-10 04:52:07.123Z | 15.716° NNE | 42.015° | 2026-02-10 04:55:07.123Z | 351.33° N |
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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