HJS-7D, 65620
Orbit data source: Space-Track
HJS-7D, 65620 is a payload satellite owned by Zhongguo Xingwang (CN) in LEO that was launched on Tue, 16 Sep 2025 UTC via a CHANG ZHENG 2C/YZ-1S 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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65620 intel report (Beta)
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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: 10 hours ago
TLE from 10 hours ago
0 HJS-7D
1 65620U 25209D 26171.42006833 -.00000067 00000-0 11006-3 0 9995
2 65620 50.0016 346.7072 0004962 51.3589 308.7732 13.41473328 38078Epoch: 2026-06-20T10:04Z
TLE epoch observation values (Epoch: 2026-06-20T10:04:53.903Z)
Latitude
-0.00003°
Longitude
-73.15237°
Altitude
1,101.981 km
Speed
7.304 km/s
True Right ascension
23h 06m 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
07:18:50
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,108.218 km
Perigee altitude
1,100.792 km
Semi-major axis
7,482.642 km
Eccentricity
0.0005
Inclination
50.0016°
RAAN
346.7072°
Arg. of periapsis
51.3589°
True anomaly
308.72885°
Mean anomaly
308.7732°
Eccentric anomaly
308.75103°
Mean motion
3.35321 °/min
Orbital period
107.36 mins
BSTAR
0.00011006
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Other satellites on launch #209 in the year 2025 (2025-09-16 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-7D 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. |
|---|---|---|---|---|---|---|---|
| 14 mins | 2026-06-20 21:19:05.167Z | 301.871° NW | 2026-06-20 21:26:05.167Z | 222.233° SW | 44.057° | 2026-06-20 21:33:05.167Z | 134.65° SE |
| 7 mins | 2026-06-20 23:15:05.167Z | 262.324° W | 2026-06-20 23:18:05.167Z | 232.341° WSW | 17.888° | 2026-06-20 23:22:05.167Z | 196.067° SSW |
| 10 mins | 2026-06-21 13:02:05.167Z | 178.41° S | 2026-06-21 13:07:05.167Z | 123.109° SE | 25.433° | 2026-06-21 13:12:05.167Z | 75.289° E |
| 12 mins | 2026-06-21 14:53:05.167Z | 239.184° WSW | 2026-06-21 14:59:05.167Z | 14.03° NNE | 44.496° | 2026-06-21 15:05:05.167Z | 54.986° ENE |
| 11 mins | 2026-06-21 16:47:05.167Z | 286.555° WNW | 2026-06-21 16:52:05.167Z | 348.486° N | 32.935° | 2026-06-21 16:58:05.167Z | 54.911° ENE |
| 11 mins | 2026-06-21 18:41:05.167Z | 310.086° NW | 2026-06-21 18:46:05.167Z | 12.41° NNE | 33.077° | 2026-06-21 18:52:05.167Z | 78.739° 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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