HJS-7A, 65617
Orbit data source: Space-Track
HJS-7A, 65617 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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65617 intel report (Beta)
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Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
ZHSW
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: 15 hours ago
TLE from 15 hours ago
0 HJS-7A
1 65617U 25209A 26171.20638559 -.00000099 00000-0 52266-4 0 9992
2 65617 50.0006 348.2358 0000993 99.7429 260.3561 13.41464125 38074Epoch: 2026-06-20T04:57Z
TLE epoch observation values (Epoch: 2026-06-20T04:57:11.714Z)
Latitude
-0.00001°
Longitude
5.51265°
Altitude
1,104.464 km
Speed
7.301 km/s
True Right ascension
23h 12m 56s
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
07:18:52
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,105.283 km
Perigee altitude
1,103.797 km
Semi-major axis
7,482.677 km
Eccentricity
0.0001
Inclination
50.0006°
RAAN
348.2358°
Arg. of periapsis
99.7429°
True anomaly
260.34488°
Mean anomaly
260.3561°
Eccentric anomaly
260.35049°
Mean motion
3.35319 °/min
Orbital period
107.36 mins
BSTAR
0.000052266
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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-7A 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 | 2026-06-20 21:34:06.932Z | 300.123° NW | 2026-06-20 21:41:06.932Z | 205.32° SW | 42.432° | 2026-06-20 21:47:06.932Z | 140.722° SSE |
| 6 mins | 2026-06-20 23:30:06.932Z | 257.749° W | 2026-06-20 23:32:06.932Z | 239.222° WSW | 15.075° | 2026-06-20 23:36:06.932Z | 203.824° SW |
| 11 mins | 2026-06-21 13:16:06.932Z | 186.993° SSW | 2026-06-21 13:21:06.932Z | 133.058° SE | 28.768° | 2026-06-21 13:27:06.932Z | 71.408° E |
| 12 mins | 2026-06-21 15:08:06.932Z | 245.227° WSW | 2026-06-21 15:13:06.932Z | 302.903° NW | 43.792° | 2026-06-21 15:20:06.932Z | 54.298° ENE |
| 11 mins | 2026-06-21 17:02:06.932Z | 291.033° WNW | 2026-06-21 17:07:06.932Z | 354.299° N | 32.164° | 2026-06-21 17:13:06.932Z | 57.128° ENE |
| 11 mins | 2026-06-21 18:56:06.932Z | 312.105° NW | 2026-06-21 19:01:06.932Z | 18.678° NNE | 34.035° | 2026-06-21 19:07:06.932Z | 83.021° 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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