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 26308.49613699 .00001016 00000-0 50747-4 0 9992
2 62079 97.4379 313.8250 0001596 88.0494 272.0924 15.19720781107758Epoch: 2026-11-04T11:54Z
TLE epoch observation values (Epoch: 2026-11-04T11:54:26.235Z)
Latitude
-0.00002°
Longitude
91.47207°
Altitude
509.733 km
Speed
7.609 km/s
True Right ascension
20h 55m 18s
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
18:50:21
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
504.75 km
Perigee altitude
502.553 km
Semi-major axis
6,881.788 km
Eccentricity
0.00016
Inclination
97.4379°
RAAN
313.825°
Arg. of periapsis
88.0494°
True anomaly
272.07412°
Mean anomaly
272.0924°
Eccentric anomaly
272.08326°
Mean motion
3.80182 °/min
Orbital period
94.69 mins
BSTAR
0.000050747
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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 | 2026-11-07 00:05:11.046Z | 139.614° SSE | 2026-11-07 00:08:11.046Z | 78.316° E | 37.74° | 2026-11-07 00:11:11.046Z | 8.324° NNE |
| 6 mins | 2026-11-07 13:10:11.046Z | 23.658° NE | 2026-11-07 13:13:11.046Z | 131.028° SE | 55.737° | 2026-11-07 13:16:11.046Z | 180.401° SSW |
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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