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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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 26141.95470498 .00000501 00000-0 63986-4 0 9993
2 45024 86.3922 127.3254 0015954 91.1439 269.1610 14.79097850342040Epoch: 2026-05-21T22:54Z
TLE epoch observation values (Epoch: 2026-05-21T22:54:46.510Z)
Latitude
0.00003°
Longitude
-95.96088°
Altitude
635.469 km
Speed
7.54 km/s
True Right ascension
08h 29m 18s
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
14:08:46
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
640.254 km
Perigee altitude
617.895 km
Semi-major axis
7,007.212 km
Eccentricity
0.0016
Inclination
86.3922°
RAAN
127.3254°
Arg. of periapsis
91.1439°
True anomaly
268.97821°
Mean anomaly
269.161°
Eccentric anomaly
269.0696°
Mean motion
3.7002 °/min
Orbital period
97.29 mins
BSTAR
0.000063986
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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 | 2026-05-22 10:50:50.816Z | 11.556° NNE | 2026-05-22 10:54:50.816Z | 105.622° ESE | 36.5° | 2026-05-22 10:57:50.816Z | 157.116° SSE |
| 7 mins | 2026-05-22 23:23:50.816Z | 169.223° S | 2026-05-22 23:26:50.816Z | 91.344° ESE | 42.827° | 2026-05-22 23:30:50.816Z | 8.476° NNE |
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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Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in descending order |
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