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: 1 day ago
TLE from 1 day ago
0 SUPERVIEW NEO-2 03
1 62079U 24218B 25260.85416474 .00004207 00000-0 20010-3 0 9994
2 62079 97.4390 267.1070 0001659 87.8104 272.3321 15.19720508 45085Epoch: 2025-09-17T20:29Z
TLE epoch observation values (Epoch: 2025-09-17T20:29:59.833Z)
Latitude
-0.00001°
Longitude
-37.41645°
Altitude
509.727 km
Speed
7.609 km/s
True Right ascension
17h 48m 25s
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
14:27:24
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
504.794 km
Perigee altitude
502.511 km
Semi-major axis
6,881.789 km
Eccentricity
0.00017
Inclination
97.439°
RAAN
267.107°
Arg. of periapsis
87.8104°
True anomaly
272.3131°
Mean anomaly
272.3321°
Eccentric anomaly
272.3226°
Mean motion
3.80182 °/min
Orbital period
94.69 mins
BSTAR
0.0002001
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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 | 2025-09-19 01:04:40.076Z | 205.836° SW | 2025-09-19 01:06:40.076Z | 251.421° W | 28.486° | 2025-09-19 01:09:40.076Z | 323.203° NNW |
| 4 mins | 2025-09-19 12:35:40.076Z | 57.689° ENE | 2025-09-19 12:37:40.076Z | 99.569° ESE | 19.423° | 2025-09-19 12:39:40.076Z | 137.777° SSE |
| 4 mins | 2025-09-19 14:09:40.076Z | 326.013° NNW | 2025-09-19 14:11:40.076Z | 279.782° WNW | 21.026° | 2025-09-19 14:13:40.076Z | 242.498° WSW |
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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