XINZHENGCHENG 02, 68412
Orbit data source: Space-Track
XINZHENGCHENG 02, 68412 is a payload satellite owned by IMI/CAS (CN) 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). Payload-class satellites include a variety of spacecraft equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.
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68412 intel report (Beta)
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Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
IMI/CAS
Mission
Operational spacecraft
Bus & Motor
QINGZHOU, Unknown motor
Mass
4,200 kg wet, ~4,200 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Unknown shape, 2.7 m
Radar Cross Section
Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 11 hours ago
TLE from 11 hours ago
0 XINZHENGCHENG 02
1 68412U 26066A 26171.38905049 .00000405 00000-0 40359-4 0 9990
2 68412 84.9663 225.7072 0023583 239.5758 120.3135 14.88410981 12208Epoch: 2026-06-20T09:20Z
TLE epoch observation values (Epoch: 2026-06-20T09:20:13.962Z)
Latitude
-0.00005°
Longitude
177.04464°
Altitude
614.344 km
Speed
7.547 km/s
True Right ascension
15h 02m 49s
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
07:18:35
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
616.28 km
Perigee altitude
583.367 km
Semi-major axis
6,977.961 km
Eccentricity
0.00236
Inclination
84.9663°
RAAN
225.7072°
Arg. of periapsis
239.5758°
True anomaly
120.54645°
Mean anomaly
120.3135°
Eccentric anomaly
120.43001°
Mean motion
3.72349 °/min
Orbital period
96.68 mins
BSTAR
0.000040359
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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.XINZHENGCHENG 02 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 | 2026-06-21 03:13:49.982Z | 116.574° SE | 2026-06-21 03:15:49.982Z | 86.619° E | 16.095° | 2026-06-21 03:17:49.982Z | 54.879° ENE |
| 6 mins | 2026-06-21 04:50:49.982Z | 226.891° WSW | 2026-06-21 04:52:49.982Z | 275.355° WNW | 31.406° | 2026-06-21 04:56:49.982Z | 346.741° N |
| 6 mins | 2026-06-21 14:57:49.982Z | 31.302° NE | 2026-06-21 14:59:49.982Z | 68.347° E | 24.765° | 2026-06-21 15:03:49.982Z | 138.189° SSE |
| 4 mins | 2026-06-21 16:35:49.982Z | 303.299° NW | 2026-06-21 16:36:49.982Z | 285.03° WNW | 19.816° | 2026-06-21 16:39:49.982Z | 232.735° WSW |
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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