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: 8 hours ago
TLE from 8 hours ago
0 YINHE-1
1 45024U 20004A 26036.95248429 .00001426 00000-0 18949-3 0 9998
2 45024 86.3988 174.4631 0015629 98.1948 262.1046 14.78954081326523Epoch: 2026-02-05T22:51Z
TLE epoch observation values (Epoch: 2026-02-05T22:51:34.642Z)
Latitude
-0.00003°
Longitude
55.47143°
Altitude
637.264 km
Speed
7.539 km/s
True Right ascension
11h 37m 51s
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
08:51:42
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
640.481 km
Perigee altitude
618.577 km
Semi-major axis
7,007.666 km
Eccentricity
0.00156
Inclination
86.3988°
RAAN
174.4631°
Arg. of periapsis
98.1948°
True anomaly
261.92725°
Mean anomaly
262.1046°
Eccentric anomaly
262.01592°
Mean motion
3.69984 °/min
Orbital period
97.3 mins
BSTAR
0.00018949
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-02-06 08:44:29.773Z | 124.333° SE | 2026-02-06 08:47:29.773Z | 74.714° E | 19.388° | 2026-02-06 08:49:29.773Z | 43.063° NE |
| 5 mins | 2026-02-06 10:22:29.773Z | 233.801° WSW | 2026-02-06 10:24:29.773Z | 276.512° WNW | 26.826° | 2026-02-06 10:27:29.773Z | 333.175° NNW |
| 6 mins | 2026-02-06 20:33:29.773Z | 34.157° NE | 2026-02-06 20:35:29.773Z | 74.648° E | 26.841° | 2026-02-06 20:39:29.773Z | 143.23° SSE |
| 4 mins | 2026-02-06 22:11:29.773Z | 307.939° NW | 2026-02-06 22:13:29.773Z | 272.154° WNW | 19.303° | 2026-02-06 22:15:29.773Z | 239.67° WSW |
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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