YINHE-1, 45024
Orbit data source: Space-Track
YINHE-1, 45024 is a payload satellite owned by Yinhe (CN) in LEO that was launched on Thu, 16 Jan 2020 UTC via a KUAIZHOU-1A 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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45024 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
Yinhe
Mission
Operational Commercial Communications
Bus & Motor
YH, Unknown motor
Mass
227 kg wet, ~200 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 1 Pan, Unknown HBR
Radar Cross Section
3.313 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 10 hours ago
TLE from 10 hours ago
0 YINHE-1
1 45024U 20004A 25311.82327068 .00001815 00000-0 24330-3 0 9999
2 45024 86.3979 214.9084 0015719 60.0252 300.2526 14.78749031313206Epoch: 2025-11-07T19:45Z
TLE epoch observation values (Epoch: 2025-11-07T19:45:30.586Z)
Latitude
-0.00008°
Longitude
-128.73075°
Altitude
630.849 km
Speed
7.546 km/s
True Right ascension
14h 19m 38s
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
02:14:52
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
641.194 km
Perigee altitude
619.161 km
Semi-major axis
7,008.314 km
Eccentricity
0.00157
Inclination
86.3979°
RAAN
214.9084°
Arg. of periapsis
60.0252°
True anomaly
300.09685°
Mean anomaly
300.2526°
Eccentric anomaly
300.17474°
Mean motion
3.69933 °/min
Orbital period
97.31 mins
BSTAR
0.0002433
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Other satellites on launch #4 in the year 2020 (2020-01-16 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.YINHE-1 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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2025-11-08 06:04:36.216Z | 349.649° N | 2025-11-08 06:07:36.216Z | 300.274° NW | 41.87° | 2025-11-08 06:11:36.216Z | 189.691° SSW |
| 7 mins | 2025-11-08 18:37:36.216Z | 206.573° SW | 2025-11-08 18:40:36.216Z | 277.34° WNW | 36.817° | 2025-11-08 18:44:36.216Z | 350.119° N |
| 5 mins | 2025-11-09 04:49:36.216Z | 42.325° NE | 2025-11-09 04:51:36.216Z | 74.949° E | 18.919° | 2025-11-09 04:54:36.216Z | 121.96° SE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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