SUPERVIEW NEO-2 03, 62079
Orbit data source: Space-Track
SUPERVIEW NEO-2 03, 62079 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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62079 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: 2 days ago
TLE from 2 days ago
0 SUPERVIEW NEO-2 03
1 62079U 24218B 26314.48790244 .00001189 00000-0 58815-4 0 9995
2 62079 97.4384 319.7289 0001611 87.3124 272.8295 15.19722654108662Epoch: 2026-11-10T11:42Z
TLE epoch observation values (Epoch: 2026-11-10T11:42:34.770Z)
Latitude
-0.00007°
Longitude
94.43465°
Altitude
509.713 km
Speed
7.609 km/s
True Right ascension
21h 18m 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
14:42:34
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
504.754 km
Perigee altitude
502.537 km
Semi-major axis
6,881.783 km
Eccentricity
0.00016
Inclination
97.4384°
RAAN
319.7289°
Arg. of periapsis
87.3124°
True anomaly
272.81106°
Mean anomaly
272.8295°
Eccentric anomaly
272.82028°
Mean motion
3.80182 °/min
Orbital period
94.69 mins
BSTAR
0.000058815
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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 03 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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-11-12 23:53:29.632Z | 129.796° SE | 2026-11-12 23:56:29.632Z | 75.118° E | 27.27° | 2026-11-12 23:59:29.632Z | 14.84° NNE |
| 5 mins | 2026-11-13 12:59:29.632Z | 46.754° ENE | 2026-11-13 13:01:29.632Z | 118.947° SE | 38.876° | 2026-11-13 13:04:29.632Z | 169.876° S |
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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