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: 6 hours ago
TLE from 6 hours ago
0 YINHE-1
1 45024U 20004A 25258.97087850 .00000737 00000-0 97147-4 0 9996
2 45024 86.3911 238.6328 0011415 235.0910 124.9239 14.78599367305398Epoch: 2025-09-15T23:18Z
TLE epoch observation values (Epoch: 2025-09-15T23:18:03.902Z)
Latitude
0.00004°
Longitude
-106.05134°
Altitude
641.452 km
Speed
7.535 km/s
True Right ascension
15h 54m 31s
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
22:22:18
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
638.651 km
Perigee altitude
622.65 km
Semi-major axis
7,008.788 km
Eccentricity
0.00114
Inclination
86.3911°
RAAN
238.6328°
Arg. of periapsis
235.091°
True anomaly
125.03106°
Mean anomaly
124.9239°
Eccentric anomaly
124.97749°
Mean motion
3.69895 °/min
Orbital period
97.32 mins
BSTAR
0.000097147
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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 | 2025-09-16 11:15:03.219Z | 343.615° N | 2025-09-16 11:18:03.219Z | 278.105° WNW | 39.142° | 2025-09-16 11:22:03.219Z | 195.647° SSW |
| 4 mins | 2025-09-16 22:12:03.219Z | 102.833° ESE | 2025-09-16 22:13:03.219Z | 87.505° E | 15.664° | 2025-09-16 22:16:03.219Z | 44.116° NE |
| 6 mins | 2025-09-16 23:48:03.219Z | 215.695° SW | 2025-09-16 23:51:03.219Z | 285.686° WNW | 32.911° | 2025-09-16 23:54:03.219Z | 341.669° N |
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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