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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Edit Public Description
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, 0.3 m
Radar Cross Section
0.375 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 SUPERVIEW NEO-2 04
1 62080U 24218C 25308.65662618 .00003026 00000-0 14485-3 0 9997
2 62080 97.4384 314.2256 0001368 110.9592 249.1790 15.19721926 52340Epoch: 2025-11-04T15:45Z
TLE epoch observation values (Epoch: 2025-11-04T15:45:32.501Z)
Latitude
0.00001°
Longitude
33.69966°
Altitude
510.104 km
Speed
7.609 km/s
True Right ascension
20h 56m 54s
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
12:32:30
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
504.589 km
Perigee altitude
502.706 km
Semi-major axis
6,881.785 km
Eccentricity
0.00014
Inclination
97.4384°
RAAN
314.2256°
Arg. of periapsis
110.9592°
True anomaly
249.16435°
Mean anomaly
249.179°
Eccentric anomaly
249.17167°
Mean motion
3.80182 °/min
Orbital period
94.69 mins
BSTAR
0.00014485
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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
Loading observer location...
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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2025-11-05 23:31:20.559Z | 101.396° ESE | 2025-11-05 23:33:20.559Z | 67.789° E | 14.424° | 2025-11-05 23:35:20.559Z | 33.844° NE |
| 4 mins | 2025-11-06 01:05:20.559Z | 215.89° SW | 2025-11-06 01:07:20.559Z | 276.447° WNW | 28.281° | 2025-11-06 01:09:20.559Z | 319.964° NNW |
| 4 mins | 2025-11-06 14:09:20.559Z | 331.034° NNW | 2025-11-06 14:11:20.559Z | 287.892° WNW | 21.362° | 2025-11-06 14:13:20.559Z | 246.549° WSW |
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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