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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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: 2 days ago
TLE from 2 days ago
0 SUPERVIEW NEO-2 03
1 62079U 24218B 25258.81300850 .00004470 00000-0 21236-3 0 9990
2 62079 97.4393 265.0946 0001647 89.0194 271.1230 15.19727026 44770Epoch: 2025-09-15T19:30Z
TLE epoch observation values (Epoch: 2025-09-15T19:30:43.934Z)
Latitude
0.00002°
Longitude
-22.60074°
Altitude
509.732 km
Speed
7.609 km/s
True Right ascension
17h 40m 22s
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
18:06:37
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
504.766 km
Perigee altitude
502.499 km
Semi-major axis
6,881.77 km
Eccentricity
0.00016
Inclination
97.4393°
RAAN
265.0946°
Arg. of periapsis
89.0194°
True anomaly
271.10413°
Mean anomaly
271.123°
Eccentric anomaly
271.11357°
Mean motion
3.80183 °/min
Orbital period
94.69 mins
BSTAR
0.00021236
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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
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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-09-18 01:22:12.243Z | 219.869° SW | 2025-09-18 01:24:12.243Z | 255.608° W | 18.96° | 2025-09-18 01:27:12.243Z | 312.65° NW |
| 5 mins | 2025-09-18 12:53:12.243Z | 46° ENE | 2025-09-18 12:55:12.243Z | 101.299° ESE | 29.104° | 2025-09-18 12:58:12.243Z | 162.206° S |
| 5 mins | 2025-09-19 01:05:12.243Z | 214.364° SW | 2025-09-19 01:07:12.243Z | 273.484° WNW | 28.51° | 2025-09-19 01:10:12.243Z | 328.151° 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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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