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). Payload-class satellites include a variety of spacecraft 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)
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Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
DFH
Mission
Operational Commercial Radar Imaging
Bus & Motor
SIWEI, Unknown motor
Mass
600 kg wet, ~500 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 0.4 m
Radar Cross Section
0.375 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 10 hours ago
TLE from 10 hours ago
0 SUPERVIEW NEO-2 04
1 62080U 24218C 26294.86651029 .00002950 00000-0 14123-3 0 9993
2 62080 97.4386 300.3958 0001454 95.2078 264.9323 15.19731152105682Epoch: 2026-10-21T20:47Z
TLE epoch observation values (Epoch: 2026-10-21T20:47:46.489Z)
Latitude
0.00002°
Longitude
-41.85752°
Altitude
509.83 km
Speed
7.609 km/s
True Right ascension
20h 01m 34s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
02:03:44
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
504.621 km
Perigee altitude
502.619 km
Semi-major axis
6,881.757 km
Eccentricity
0.00015
Inclination
97.4386°
RAAN
300.3958°
Arg. of periapsis
95.2078°
True anomaly
264.9157°
Mean anomaly
264.9323°
Eccentric anomaly
264.924°
Mean motion
3.80184 °/min
Orbital period
94.69 mins
BSTAR
0.00014123
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Other satellites on launch #218 in the year 2024 (2024-11-24 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.SUPERVIEW NEO-2 04 Visibility forecast
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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 | 2026-10-22 13:09:18.128Z | 20.052° NNE | 2026-10-22 13:13:18.128Z | 137.708° SSE | 53.508° | 2026-10-22 13:16:18.128Z | 180.737° SSW |
| 4 mins | 2026-10-22 23:49:18.128Z | 104.724° ESE | 2026-10-22 23:51:18.128Z | 57.454° ENE | 22.793° | 2026-10-22 23:53:18.128Z | 21.423° NNE |
| 4 mins | 2026-10-23 01:23:18.128Z | 236.553° WSW | 2026-10-23 01:24:18.128Z | 257.798° W | 20.448° | 2026-10-23 01:27:18.128Z | 313.718° NW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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