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, 0.3 m
Radar Cross Section
0.375 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 12 hours ago
TLE from 12 hours ago
0 SUPERVIEW NEO-2 03
1 62079U 24218B 26130.45493345 .00000008 00000-0 35382-5 0 9994
2 62079 97.4393 138.3214 0001627 88.2343 271.9078 15.19713194 80718Epoch: 2026-05-10T10:55Z
TLE epoch observation values (Epoch: 2026-05-10T10:55:06.250Z)
Latitude
-0.00002°
Longitude
106.28759°
Altitude
509.759 km
Speed
7.609 km/s
True Right ascension
09h 13m 17s
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
06:49:31
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
504.794 km
Perigee altitude
502.555 km
Semi-major axis
6,881.811 km
Eccentricity
0.00016
Inclination
97.4393°
RAAN
138.3214°
Arg. of periapsis
88.2343°
True anomaly
271.88917°
Mean anomaly
271.9078°
Eccentric anomaly
271.89848°
Mean motion
3.8018 °/min
Orbital period
94.69 mins
BSTAR
0.0000035382
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-05-10 23:43:02.701Z | 107.012° ESE | 2026-05-10 23:45:02.701Z | 66.899° ENE | 18.94° | 2026-05-10 23:47:02.701Z | 28.628° NE |
| 4 mins | 2026-05-11 01:17:02.701Z | 226.498° WSW | 2026-05-11 01:19:02.701Z | 273.937° WNW | 21.807° | 2026-05-11 01:21:02.701Z | 312.66° NW |
| 5 mins | 2026-05-11 12:47:02.701Z | 46.371° ENE | 2026-05-11 12:49:02.701Z | 91.745° ESE | 25.543° | 2026-05-11 12:52:02.701Z | 154.87° SSE |
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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