SUPERVIEW NEO-2 04, 62080
Orbit data source: Space-Track
SUPERVIEW NEO-2 04, 62080 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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62080 intel report (Beta)
SUPERVIEW NEO-2 04 details
| Identifier | |
| Orbit | SSO |
| Last TLE update | 2 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 2 days ago
0 SUPERVIEW NEO-2 04
1 62080U 24218C 24346.62365491 .00000517 00000-0 27386-4 0 9991
2 62080 97.4393 350.8784 0001740 87.6374 272.5060 15.19722620 2521Epoch: 2024-12-11T14:58Z
Definitive object data (Epoch: 2024-12-11T14:58:03.784Z)
| Latitude | -0.00001° |
| Longitude | 45.54696° |
| Altitude | 509.715 km |
| Speed | 7.609 km/s |
| True Right ascension | 23h 23m 30s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
| Latitude | -82.56012° |
| Longitude | 143.84754° |
| Altitude | 536.247 km |
| Speed | 7.593 km/s |
| Apparent Right ascension | 08h 02m 29s |
| Apparent Declination | -62° 38' 36" |
| Sunlit | Object is in daylight |
Visualization observer readout
| Local Sidereal Time | 20:24:26 |
| Azimuth | 173.533° S |
| Elevation | -67.035° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 504.843 km |
| Perigee altitude | 502.448 km |
| Semi-major axis | 6,881.783 km |
| Eccentricity | 0.000174 |
| Inclination | 97.4393° |
| RAAN | 350.8784° |
| Arg. of periapsis | 87.6374° |
| True anomaly | 272.48608° |
| Mean anomaly | 272.506° |
| Eccentric anomaly | 272.49604° |
| Mean motion | 3.80182 °/min |
| BSTAR | 0.000027386 |
| 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 04 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 23:59:37.483Z | 131.874° SE | 2024-12-14 00:02:37.483Z | 64.696° ENE | 27.7° | 2024-12-14 00:05:37.483Z | 9.021° NNE |
| 5 mins | 2024-12-14 13:04:37.483Z | 32.094° NE | 2024-12-14 13:06:37.483Z | 87.129° E | 36.672° | 2024-12-14 13:09:37.483Z | 171.592° S |
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