HULIANWANG DIGUI-157, 68131
Orbit data source: Space-Track
HULIANWANG DIGUI-157, 68131 is a payload satellite owned by Zhongguo Xingwang (CN) in LEO that was launched on Thu, 12 Mar 2026 UTC via a CHANG ZHENG 8A launch vehicle from the Wenchang Satellite Launch Center (WSC). 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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68131 intel report (Beta)
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Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
CAST?
Mission
Operational spacecraft
Bus & Motor
XINGWANG C, Unknown motor
Mass
~700 kg wet, ~700 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Unknown shape, 1.1 m
Radar Cross Section
RCS unknown
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 HULIANWANG DIGUI-157
1 68131U 26047C 26118.56920610 -.00000127 00000-0 31540-5 0 9994
2 68131 50.0038 234.6254 0001469 287.7108 72.3611 13.44273479 6466Epoch: 2026-04-28T13:39Z
TLE epoch observation values (Epoch: 2026-04-28T13:39:39.407Z)
Latitude
0.00006°
Longitude
173.16862°
Altitude
1,093.58 km
Speed
7.307 km/s
True Right ascension
15h 38m 30s
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
21:31:54
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,095.21 km
Perigee altitude
1,093.015 km
Semi-major axis
7,472.249 km
Eccentricity
0.00015
Inclination
50.0038°
RAAN
234.6254°
Arg. of periapsis
287.7108°
True anomaly
72.37714°
Mean anomaly
72.3611°
Eccentric anomaly
72.36912°
Mean motion
3.36021 °/min
Orbital period
107.14 mins
BSTAR
0.000003154
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Other satellites on launch #47 in the year 2026 (2026-03-12 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.HULIANWANG DIGUI-157 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. |
|---|---|---|---|---|---|---|---|
| 13 mins | 2026-04-29 15:03:12.291Z | 305.68° NW | 2026-04-29 15:09:12.291Z | 7.589° NNE | 34.357° | 2026-04-29 15:16:12.291Z | 86.401° E |
| 12 mins | 2026-04-29 16:57:12.291Z | 302.509° NW | 2026-04-29 17:02:12.291Z | 259.923° W | 44.662° | 2026-04-29 17:09:12.291Z | 129.871° SE |
| 9 mins | 2026-04-29 18:50:12.291Z | 272.392° WNW | 2026-04-29 18:54:12.291Z | 231.968° WSW | 20.554° | 2026-04-29 18:59:12.291Z | 186.13° SSW |
| 9 mins | 2026-04-30 08:37:12.291Z | 167.84° S | 2026-04-30 08:41:12.291Z | 125.548° SE | 22.008° | 2026-04-30 08:46:12.291Z | 78.649° E |
| 12 mins | 2026-04-30 10:27:12.291Z | 232.642° WSW | 2026-04-30 10:33:12.291Z | 66.08° ENE | 44.507° | 2026-04-30 10:39:12.291Z | 56.435° ENE |
| 12 mins | 2026-04-30 12:20:12.291Z | 279.793° WNW | 2026-04-30 12:25:12.291Z | 334.922° NNW | 33.683° | 2026-04-30 12:32:12.291Z | 55.34° ENE |
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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