OBJECT A, 68412
Orbit data source: Space-Track
OBJECT A, 68412 is a Chinese satellite in LEO that was launched on Mon, 30 Mar 2026 UTC via a LIJIAN-2 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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68412 intel report (Beta)
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Identifier
Orbit
Country
CN / PRCRelated business
None
Manufacturer
Unknown
Mission
Spacecraft
Bus & Motor
Unknown
Mass
Unknown
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: 22 hours ago
TLE from 22 hours ago
0 OBJECT A
1 68412U 26066A 26090.86061244 .00027820 00000-0 49494-3 0 9991
2 68412 84.9606 276.9718 0206090 144.2419 217.2835 15.29824820 221Epoch: 2026-03-31T20:39Z
TLE epoch observation values (Epoch: 2026-03-31T20:39:16.914Z)
Latitude
-0.00004°
Longitude
137.91959°
Altitude
592.965 km
Speed
7.501 km/s
True Right ascension
18h 27m 53s
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
00:07:36
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
614.4 km
Perigee altitude
332.001 km
Semi-major axis
6,851.338 km
Eccentricity
0.02061
Inclination
84.9606°
RAAN
276.9718°
Arg. of periapsis
144.2419°
True anomaly
215.88182°
Mean anomaly
217.2835°
Eccentric anomaly
216.57981°
Mean motion
3.82719 °/min
Orbital period
94.06 mins
BSTAR
0.00049494
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Other satellites on launch #66 in the year 2026 (2026-03-30 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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-04-01 23:54:34.676Z | 27.084° NE | 2026-04-01 23:56:34.676Z | 81.994° E | 22.24° | 2026-04-01 23:58:34.676Z | 135.93° SSE |
| 4 mins | 2026-04-02 13:37:34.676Z | 243.22° WSW | 2026-04-02 13:39:34.676Z | 291.519° WNW | 21.598° | 2026-04-02 13:41:34.676Z | 330.039° NNW |
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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