SUPERVIEW NEO-2 03, 62079
Orbit data source: Space-Track
SUPERVIEW NEO-2 03, 62079 is a payload satellite owned by Siwei (CN) in SSO that was launched on Sun, 24 Nov 2024 UTC via a CHANG ZHENG 2C 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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62079 intel report (Beta)
SUPERVIEW NEO-2 03 details
| Identifier | |
| Orbit | SSO |
| Last TLE update | 3 days ago |
| Origin | |
| Manufacturer | DFH |
| Mission | Operational spacecraft |
| Bus & Motor | SIWEI, Unknown motor |
| Mass | 600 kg wet, ~500 kg dry |
| Launch date (UTC) | |
| Launch vehicle | |
| Launch site | |
| Object type | Payload Rocket body Debris |
| Shape & HBR | Unknown |
| Radar Cross Section | Large (>1 m²) |
Expand to show TLE details & history
TLE from 3 days ago
0 SUPERVIEW NEO-2 03
1 62079U 24218B 24346.03112663 -.00000006 00000-0 28849-5 0 9995
2 62079 97.4393 350.3170 0001710 87.4278 272.7153 15.19720801 2435Epoch: 2024-12-11T00:44Z
Definitive object data (Epoch: 2024-12-11T00:44:49.34Z)
| Latitude | -0.00001° |
| Longitude | -101.12024° |
| Altitude | 509.717 km |
| Speed | 7.609 km/s |
| True Right ascension | 23h 21m 16s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
| Latitude | -46.20514° |
| Longitude | 73.92701° |
| Altitude | 525.614 km |
| Speed | 7.598 km/s |
| Apparent Right ascension | 09h 36m 19s |
| Apparent Declination | -44° 58' 26" |
| Sunlit | Object is in daylight |
Visualization observer readout
| Local Sidereal Time | 20:13:14 |
| Azimuth | 244.873° WSW |
| Elevation | -73.913° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 504.828 km |
| Perigee altitude | 502.475 km |
| Semi-major axis | 6,881.788 km |
| Eccentricity | 0.000171 |
| Inclination | 97.4393° |
| RAAN | 350.317° |
| Arg. of periapsis | 87.4278° |
| True anomaly | 272.69573° |
| Mean anomaly | 272.7153° |
| Eccentric anomaly | 272.70551° |
| Mean motion | 3.80182 °/min |
| BSTAR | 0.0000028849 |
| Orbital period | 94.69 mins |
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Other satellites on launch #218 in the year 2024 (2024-11-24 UTC)
| CZ-2C R/B, 62078 |
| SUPERVIEW NEO-2 03, 62079 |
| SUPERVIEW NEO-2 04, 62080 |
SUPERVIEW NEO-2 03 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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2024-12-13 23:59:27.333Z | 134.11° SE | 2024-12-14 00:02:27.333Z | 74.105° E | 27.86° | 2024-12-14 00:05:27.333Z | 11.062° NNE |
| 6 mins | 2024-12-14 13:04:27.333Z | 29.723° NE | 2024-12-14 13:06:27.333Z | 72.547° E | 35.446° | 2024-12-14 13:10:27.333Z | 175.416° S |
Authenticating...
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