CHINASAT 4A, 60606
Orbit data source: Space-Track
CHINASAT 4A, 60606 is a payload satellite owned by PLA SSF (CN) in GEO that was launched on Thu, 22 Aug 2024 UTC via a CHANG ZHENG 7A launch vehicle from the Wenchang Satellite Launch Center (WSC). 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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60606 intel report (Beta)
CHINASAT 4A details
Identifier | |
Orbit | GEO |
Last TLE update | 17 hours ago |
Origin | |
Manufacturer | SISE |
Mission | Operational spacecraft |
Bus & Motor | FY-4?, LAE |
Mass | ~5,000 kg wet, ~2,500 kg dry |
Launch date (UTC) | |
Launch vehicle | |
Launch site | |
Object type | Payload Rocket body Debris |
Shape & HBR | Unknown |
Radar Cross Section | RCS unknown |
Expand to show TLE details & history
TLE from 17 hours ago
0 CHINASAT 4A
1 60606U 24151A 25014.63761589 -.00000361 00000-0 00000-0 0 9999
2 60606 2.6537 276.7185 0003212 22.1054 163.2294 1.00268958 1558
Epoch: 2025-01-14T15:18Z
Definitive object data (Epoch: 2025-01-14T15:18:10.012Z)
Latitude | -0.22502° |
Longitude | 118.20465° |
Altitude | 35,799.953 km |
Speed | 3.074 km/s |
True Right ascension | 06h 48m 21s |
True Declination | 0° 13' 29" |
Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
Latitude | 2.61826° |
Longitude | 16.04374° |
Altitude | 35,780.119 km |
Speed | 3.075 km/s |
Apparent Right ascension | 23h 42m 52s |
Apparent Declination | -2° 41' 02" |
Sunlit | Object is in daylight |
Visualization observer readout
Local Sidereal Time | 09:06:22 |
Azimuth | 306.2° NW |
Elevation | -38.638° |
Doppler factor | 1 |
Orbital elements
Apogee altitude | 35,801.998 km |
Perigee altitude | 35,774.911 km |
Semi-major axis | 42,166.591 km |
Eccentricity | 0.0003212 |
Inclination | 2.6537° |
RAAN | 276.7185° |
Arg. of periapsis | 22.1054° |
True anomaly | 163.24002° |
Mean anomaly | 163.2294° |
Eccentric anomaly | 163.23471° |
Mean motion | 0.25066 °/min |
BSTAR | Unknown |
Orbital period | 1436.19 mins |
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60606 neighbors
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Other satellites on launch #151 in the year 2024 (2024-08-22 UTC)
CHINASAT 4A, 60606 |
CZ-7A R/B, 60607 |
CHINASAT 4A 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. |
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