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: 10 hours ago
TLE from 10 hours ago
0 SUPERVIEW NEO-2 04
1 62080U 24218C 26040.57837780 .00003369 00000-0 16090-3 0 9990
2 62080 97.4393 49.7353 0001392 110.2936 249.8448 15.19721355 67068Epoch: 2026-02-09T13:52Z
TLE epoch observation values (Epoch: 2026-02-09T13:52:51.841Z)
Latitude
-0.00011°
Longitude
61.84813°
Altitude
510.101 km
Speed
7.609 km/s
True Right ascension
03h 18m 56s
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
02:15:57
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
504.608 km
Perigee altitude
502.692 km
Semi-major axis
6,881.787 km
Eccentricity
0.00014
Inclination
97.4393°
RAAN
49.7353°
Arg. of periapsis
110.2936°
True anomaly
249.82983°
Mean anomaly
249.8448°
Eccentric anomaly
249.83731°
Mean motion
3.80182 °/min
Orbital period
94.69 mins
BSTAR
0.0001609
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-02-10 01:04:05.956Z | 200.855° SSW | 2026-02-10 01:07:05.956Z | 270.544° WNW | 28.67° | 2026-02-10 01:10:05.956Z | 327.54° NNW |
| 4 mins | 2026-02-10 12:36:05.956Z | 66.543° ENE | 2026-02-10 12:37:05.956Z | 88.044° E | 19.326° | 2026-02-10 12:40:05.956Z | 143.995° SSE |
| 4 mins | 2026-02-10 14:10:05.956Z | 316.253° NNW | 2026-02-10 14:11:05.956Z | 292.265° WNW | 21.354° | 2026-02-10 14:14:05.956Z | 236.974° 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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