XINZHENGCHENG 01, 68414
Orbit data source: Space-Track
XINZHENGCHENG 01, 68414 is a Chinese payload 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). 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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68414 intel report (Beta)
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Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
ZHWK
Mission
Operational spacecraft
Bus & Motor
XZC1, Unknown motor
Mass
~100 kg wet, ~100 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Unknown shape, 0.8 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 XINZHENGCHENG 01
1 68414U 26066C 26170.63980788 .00000660 00000-0 67363-4 0 9999
2 68414 84.9659 226.1682 0024101 243.1283 116.7477 14.88631911 12091Epoch: 2026-06-19T15:21Z
TLE epoch observation values (Epoch: 2026-06-19T15:21:19.400Z)
Latitude
-0.00005°
Longitude
87.97147°
Altitude
612.919 km
Speed
7.549 km/s
True Right ascension
15h 04m 40s
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
07:22:04
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
615.949 km
Perigee altitude
582.317 km
Semi-major axis
6,977.27 km
Eccentricity
0.00241
Inclination
84.9659°
RAAN
226.1682°
Arg. of periapsis
243.1283°
True anomaly
116.99399°
Mean anomaly
116.7477°
Eccentric anomaly
116.87088°
Mean motion
3.72404 °/min
Orbital period
96.67 mins
BSTAR
0.000067363
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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 01 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 | 2026-06-21 04:35:18.518Z | 202.045° SSW | 2026-06-21 04:38:18.518Z | 264.292° W | 39.237° | 2026-06-21 04:42:18.518Z | 353.644° N |
| 4 mins | 2026-06-21 14:44:18.518Z | 51.573° ENE | 2026-06-21 14:45:18.518Z | 69.414° E | 18.534° | 2026-06-21 14:48:18.518Z | 118.896° SE |
| 6 mins | 2026-06-21 16:20:18.518Z | 325.052° NNW | 2026-06-21 16:23:18.518Z | 262.56° W | 26.706° | 2026-06-21 16:26:18.518Z | 213.801° SW |
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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