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: 19 hours ago
TLE from 19 hours ago
0 YINHE-1
1 45024U 20004A 25291.31909160 .00001353 00000-0 18063-3 0 9992
2 45024 86.3964 224.1067 0015502 121.3832 238.8907 14.78693443310176Epoch: 2025-10-18T07:39Z
TLE epoch observation values (Epoch: 2025-10-18T07:39:29.514Z)
Latitude
-0.00005°
Longitude
82.1819°
Altitude
642.195 km
Speed
7.534 km/s
True Right ascension
14h 56m 25s
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
21:20:09
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
641.218 km
Perigee altitude
619.489 km
Semi-major axis
7,008.49 km
Eccentricity
0.00155
Inclination
86.3964°
RAAN
224.1067°
Arg. of periapsis
121.3832°
True anomaly
238.73876°
Mean anomaly
238.8907°
Eccentric anomaly
238.81471°
Mean motion
3.69919 °/min
Orbital period
97.32 mins
BSTAR
0.00018063
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-10-19 06:58:19.972Z | 30.16° NE | 2025-10-19 07:01:19.972Z | 81.028° E | 22.727° | 2025-10-19 07:04:19.972Z | 130.876° SE |
| 5 mins | 2025-10-19 08:37:19.972Z | 308.337° NW | 2025-10-19 08:39:19.972Z | 266.383° W | 22.847° | 2025-10-19 08:42:19.972Z | 221.992° SW |
| 6 mins | 2025-10-19 19:31:19.972Z | 140.946° SSE | 2025-10-19 19:34:19.972Z | 81.214° E | 28.451° | 2025-10-19 19:37:19.972Z | 27.669° NE |
| 4 mins | 2025-10-19 21:10:19.972Z | 253.69° W | 2025-10-19 21:12:19.972Z | 288.771° WNW | 18.401° | 2025-10-19 21:14:19.972Z | 319.86° NNW |
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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