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, 0.3 m
Radar Cross Section
0.375 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 14 hours ago
TLE from 14 hours ago
0 SUPERVIEW NEO-2 04
1 62080U 24218C 26093.51664469 .00000394 00000-0 21605-4 0 9998
2 62080 97.4394 101.9125 0001394 113.6536 246.4845 15.19719398 75104Epoch: 2026-04-03T12:23Z
TLE epoch observation values (Epoch: 2026-04-03T12:23:58.101Z)
Latitude
-0.00004°
Longitude
84.07077°
Altitude
510.16 km
Speed
7.609 km/s
True Right ascension
06h 47m 39s
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
08:16:23
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
504.615 km
Perigee altitude
502.696 km
Semi-major axis
6,881.793 km
Eccentricity
0.00014
Inclination
97.4394°
RAAN
101.9125°
Arg. of periapsis
113.6536°
True anomaly
246.46985°
Mean anomaly
246.4845°
Eccentric anomaly
246.47718°
Mean motion
3.80181 °/min
Orbital period
94.69 mins
BSTAR
0.000021605
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-04-04 12:41:08.964Z | 50.085° ENE | 2026-04-04 12:43:08.964Z | 92.203° ESE | 22.334° | 2026-04-04 12:46:08.964Z | 150.177° SSE |
| 5 mins | 2026-04-05 00:53:08.964Z | 196.282° SSW | 2026-04-05 00:55:08.964Z | 262.934° W | 36.635° | 2026-04-05 00:58:08.964Z | 333.678° NNW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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