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 | 19 hours 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 19 hours ago
0 SUPERVIEW NEO-2 04
1 62080U 24218C 24360.64834038 -.00000039 00000-0 13480-5 0 9998
2 62080 97.4382 4.6988 0001727 84.5033 275.6398 15.19720187 4652Epoch: 2024-12-25T15:33Z
Definitive object data (Epoch: 2024-12-25T15:33:36.608Z)
| Latitude | -0.00013° |
| Longitude | 36.65721° |
| Altitude | 509.658 km |
| Speed | 7.609 km/s |
| True Right ascension | 00h 18m 47s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
| Latitude | 10.98351° |
| Longitude | 35.99385° |
| Altitude | 508.618 km |
| Speed | 7.611 km/s |
| Apparent Right ascension | 23h 17m 24s |
| Apparent Declination | -13° 57' 37" |
| Sunlit | Object is in daylight |
Visualization observer readout
| Local Sidereal Time | 09:55:29 |
| Azimuth | 319.556° NNW |
| Elevation | -58.44° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 504.842 km |
| Perigee altitude | 502.465 km |
| Semi-major axis | 6,881.79 km |
| Eccentricity | 0.0001727 |
| Inclination | 97.4382° |
| RAAN | 4.6988° |
| Arg. of periapsis | 84.5033° |
| True anomaly | 275.62011° |
| Mean anomaly | 275.6398° |
| Eccentric anomaly | 275.62995° |
| Mean motion | 3.80182 °/min |
| BSTAR | 0.000001348 |
| 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 | 2024-12-26 12:40:17.175Z | 40.147° NE | 2024-12-26 12:43:17.175Z | 95.707° ESE | 22.398° | 2024-12-26 12:46:17.175Z | 151.432° SSE |
| 5 mins | 2024-12-27 00:53:17.175Z | 197.886° SSW | 2024-12-27 00:55:17.175Z | 270.396° WNW | 36.427° | 2024-12-27 00:58:17.175Z | 334.368° NNW |
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