HJS-6B, 63429
Orbit data source: Space-Track
HJS-6B, 63429 is a payload satellite owned by Zhongguo Xingwang (CN) in LEO that was launched on Tue, 01 Apr 2025 UTC via a CHANG ZHENG 2D 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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63429 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
YINNT
Mission
Operational Civil Communications
Bus & Motor
Unknown
Mass
~300 kg wet, ~300 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 1.1 m
Radar Cross Section
2.320 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 6 hours ago
TLE from 6 hours ago
0 HJS-6B
1 63429U 25067B 25309.28571919 .00014850 00000-0 40432-3 0 9999
2 63429 54.9930 308.8757 0011482 112.7698 247.4544 15.37720003 33570Epoch: 2025-11-05T06:51Z
TLE epoch observation values (Epoch: 2025-11-05T06:51:26.138Z)
Latitude
-0.00005°
Longitude
161.25618°
Altitude
456.967 km
Speed
7.638 km/s
True Right ascension
20h 35m 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
09:13:11
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
460.66 km
Perigee altitude
444.973 km
Semi-major axis
6,830.954 km
Eccentricity
0.00115
Inclination
54.993°
RAAN
308.8757°
Arg. of periapsis
112.7698°
True anomaly
247.33295°
Mean anomaly
247.4544°
Eccentric anomaly
247.39367°
Mean motion
3.84433 °/min
Orbital period
93.64 mins
BSTAR
0.00040432
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Other satellites on launch #67 in the year 2025 (2025-04-01 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.HJS-6B 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-11-06 01:43:34.611Z | 178.231° S | 2025-11-06 01:46:34.611Z | 115.803° SE | 20.558° | 2025-11-06 01:48:34.611Z | 78.224° E |
| 4 mins | 2025-11-06 03:21:34.611Z | 272.405° WNW | 2025-11-06 03:23:34.611Z | 338.18° N | 29.535° | 2025-11-06 03:25:34.611Z | 24.443° NE |
| 5 mins | 2025-11-06 09:54:34.611Z | 306.17° NW | 2025-11-06 09:56:34.611Z | 172.512° S | 42.816° | 2025-11-06 09:59:34.611Z | 139.519° SSE |
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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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