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: 15 hours ago
TLE from 15 hours ago
0 SUPERVIEW NEO-2 03
1 62079U 24218B 26294.66898098 .00002853 00000-0 13673-3 0 9999
2 62079 97.4381 300.1995 0001647 89.3171 270.8253 15.19730307105652Epoch: 2026-10-21T16:03Z
TLE epoch observation values (Epoch: 2026-10-21T16:03:19.956Z)
Latitude
0.00001°
Longitude
29.25143°
Altitude
509.728 km
Speed
7.609 km/s
True Right ascension
20h 00m 47s
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
02:05:27
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
504.756 km
Perigee altitude
502.489 km
Semi-major axis
6,881.76 km
Eccentricity
0.00016
Inclination
97.4381°
RAAN
300.1995°
Arg. of periapsis
89.3171°
True anomaly
270.80643°
Mean anomaly
270.8253°
Eccentric anomaly
270.81586°
Mean motion
3.80184 °/min
Orbital period
94.69 mins
BSTAR
0.00013673
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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 | 2026-10-22 13:10:00.099Z | 22.72° NE | 2026-10-22 13:13:00.099Z | 116.786° SE | 58.612° | 2026-10-22 13:16:00.099Z | 179.732° S |
| 4 mins | 2026-10-22 23:49:00.099Z | 109.731° ESE | 2026-10-22 23:51:00.099Z | 65.105° ENE | 23.357° | 2026-10-22 23:53:00.099Z | 25.081° NE |
| 4 mins | 2026-10-23 01:23:00.099Z | 231.278° WSW | 2026-10-23 01:25:00.099Z | 274.275° WNW | 20.342° | 2026-10-23 01:27:00.099Z | 310.22° NW |
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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