OBJECT A, 68414
Orbit data source: Space-Track
OBJECT A, 68414 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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68414 intel report (Beta)
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Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
ZHWK
Mission
Spacecraft
Bus & Motor
XZC1, Unknown motor
Mass
~100 kg wet, ~100 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: 2 days ago
TLE from 2 days ago
0 OBJECT A
1 68414U 26066C 26093.80455066 .00002339 00000-0 22927-3 0 9999
2 68414 85.1331 274.8711 0065547 46.0550 314.6055 14.90103412 664Epoch: 2026-04-03T19:18Z
TLE epoch observation values (Epoch: 2026-04-03T19:18:33.177Z)
Latitude
-0.00008°
Longitude
153.09944°
Altitude
568.76 km
Speed
7.594 km/s
True Right ascension
18h 19m 29s
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
23:11:05
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
640.233 km
Perigee altitude
548.826 km
Semi-major axis
6,972.666 km
Eccentricity
0.00655
Inclination
85.1331°
RAAN
274.8711°
Arg. of periapsis
46.055°
True anomaly
314.06765°
Mean anomaly
314.6055°
Eccentric anomaly
314.33689°
Mean motion
3.72773 °/min
Orbital period
96.57 mins
BSTAR
0.00022927
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-04-05 23:26:29.341Z | 15.02° NNE | 2026-04-05 23:30:29.341Z | 98.301° ESE | 31.098° | 2026-04-05 23:33:29.341Z | 147.693° SSE |
| 5 mins | 2026-04-06 11:55:29.341Z | 132.076° SE | 2026-04-06 11:57:29.341Z | 76.039° E | 28.456° | 2026-04-06 12:00:29.341Z | 24.951° NE |
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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