HULIANWANG DIGUI-158, 68132
Orbit data source: Space-Track
HULIANWANG DIGUI-158, 68132 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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68132 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
Radar Cross Section
RCS unknown
Expand to show TLE details & historyLast TLE update: 21 hours ago
TLE from 21 hours ago
0 HULIANWANG DIGUI-158
1 68132U 26047D 26104.70090810 -.00000105 00000-0 38694-4 0 9998
2 68132 50.0073 286.6296 0002144 338.8634 21.2166 13.66629066 4571Epoch: 2026-04-14T16:49Z
TLE epoch observation values (Epoch: 2026-04-14T16:49:18.459Z)
Latitude
0°
Longitude
-168.5707°
Altitude
1,010.737 km
Speed
7.348 km/s
True Right ascension
19h 06m 31s
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
20:45:24
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,014 km
Perigee altitude
1,010.831 km
Semi-major axis
7,390.552 km
Eccentricity
0.00021
Inclination
50.0073°
RAAN
286.6296°
Arg. of periapsis
338.8634°
True anomaly
21.22549°
Mean anomaly
21.2166°
Eccentric anomaly
21.22105°
Mean motion
3.41608 °/min
Orbital period
105.38 mins
BSTAR
0.000038694
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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-158 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. |
|---|---|---|---|---|---|---|---|
| 11 mins | 2026-04-15 15:51:53.028Z | 255.133° W | 2026-04-15 15:56:53.028Z | 335.098° NNW | 41.581° | 2026-04-15 16:02:53.028Z | 52.427° ENE |
| 10 mins | 2026-04-15 17:43:53.028Z | 297.969° NW | 2026-04-15 17:47:53.028Z | 347.441° N | 29.891° | 2026-04-15 17:53:53.028Z | 57.832° ENE |
| 11 mins | 2026-04-15 19:34:53.028Z | 311.051° NW | 2026-04-15 19:39:53.028Z | 15.178° NNE | 34.452° | 2026-04-15 19:45:53.028Z | 87.179° E |
| 11 mins | 2026-04-15 21:25:53.028Z | 300.848° NW | 2026-04-15 21:30:53.028Z | 215.318° SW | 44.297° | 2026-04-15 21:36:53.028Z | 133.462° SE |
| 6 mins | 2026-04-15 23:17:53.028Z | 261.822° W | 2026-04-15 23:20:53.028Z | 229.616° WSW | 17.697° | 2026-04-15 23:23:53.028Z | 199.596° SSW |
| 7 mins | 2026-04-16 12:50:53.028Z | 154.289° SSE | 2026-04-16 12:53:53.028Z | 121.196° SE | 18.315° | 2026-04-16 12:57:53.028Z | 83.613° E |
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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