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). Payloads include a variety of satellites, spacecraft, and rockets 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)
YINHE-1 details
| Identifier | |
| Orbit | LEO |
| Last TLE update | 8 hours ago |
| Origin | |
| 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 | Payload Rocket body Debris |
| Shape & HBR | Box + 1 Pan, Unknown HBR |
| Radar Cross Section | 3.313 m², Large (>1 m²) |
Expand to show TLE details & history
TLE from 8 hours ago
0 YINHE-1
1 45024U 20004A 24361.12467998 .00001847 00000-0 25247-3 0 9996
2 45024 86.3942 357.1179 0016208 85.5314 274.7757 14.77930900266435Epoch: 2024-12-26T02:59Z
Definitive object data (Epoch: 2024-12-26T02:59:32.35Z)
| Latitude | -0.00003° |
| Longitude | -142.87547° |
| Altitude | 638.047 km |
| Speed | 7.54 km/s |
| True Right ascension | 23h 48m 28s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
| Latitude | -45.54381° |
| Longitude | 40.64646° |
| Altitude | 662.389 km |
| Speed | 7.52 km/s |
| Apparent Right ascension | 16h 53m 56s |
| Apparent Declination | -73° 00' 50" |
| Sunlit | Object is in daylight |
Visualization observer readout
| Local Sidereal Time | 09:51:39 |
| Azimuth | 157.613° S |
| Elevation | -42.363° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 644.129 km |
| Perigee altitude | 621.403 km |
| Semi-major axis | 7,010.903 km |
| Eccentricity | 0.0016208 |
| Inclination | 86.3942° |
| RAAN | 357.1179° |
| Arg. of periapsis | 85.5314° |
| True anomaly | 274.59058° |
| Mean anomaly | 274.7757° |
| Eccentric anomaly | 274.68315° |
| Mean motion | 3.69728 °/min |
| BSTAR | 0.00025247 |
| Orbital period | 97.37 mins |
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Other satellites on launch #4 in the year 2020 (2020-01-16 UTC)
| YINHE-1, 45024 |
| KZ-1A R/B, 45025 (Decayed) |
YINHE-1 Visibility forecast
Observer location: undefined°, undefined
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 | 2024-12-26 11:41:27.430Z | 17.903° NNE | 2024-12-26 11:44:27.430Z | 74.305° E | 32.969° | 2024-12-26 11:48:27.430Z | 152.185° SSE |
| 6 mins | 2024-12-27 00:15:27.430Z | 157.241° SSE | 2024-12-27 00:17:27.430Z | 108.779° ESE | 39.102° | 2024-12-27 00:21:27.430Z | 13.291° NNE |
Authenticating...
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