SUPERVIEW NEO-1 01, 52320
Orbit data source: Space-Track
SUPERVIEW NEO-1 01, 52320 is a payload satellite owned by Siwei (CN) in SSO that was launched on Fri, 29 Apr 2022 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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52320 intel report (Beta)
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Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
DFH
Mission
Operational Commercial Imaging
Bus & Motor
SIWEI, Unknown motor
Mass
540 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: 23 hours ago
TLE from 23 hours ago
0 SUPERVIEW NEO-1 01
1 52320U 22043A 26172.49897994 .00003420 00000-0 17864-3 0 9998
2 52320 97.3401 245.1413 0000297 208.3716 151.7502 15.16546212230215Epoch: 2026-06-21T11:58Z
TLE epoch observation values (Epoch: 2026-06-21T11:58:31.866Z)
Latitude
0.00003°
Longitude
155.81014°
Altitude
519.556 km
Speed
7.604 km/s
True Right ascension
16h 20m 33s
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
21:47:22
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
513.461 km
Perigee altitude
513.051 km
Semi-major axis
6,891.393 km
Eccentricity
0.00003
Inclination
97.3401°
RAAN
245.1413°
Arg. of periapsis
208.3716°
True anomaly
151.75181°
Mean anomaly
151.7502°
Eccentric anomaly
151.75101°
Mean motion
3.79387 °/min
Orbital period
94.89 mins
BSTAR
0.00017864
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Other satellites on launch #43 in the year 2022 (2022-04-29 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-1 01 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-06-22 17:03:18.747Z | 43.238° NE | 2026-06-22 17:06:18.747Z | 106.575° ESE | 23.183° | 2026-06-22 17:08:18.747Z | 145.924° SSE |
| 4 mins | 2026-06-22 18:38:18.747Z | 321.856° NNW | 2026-06-22 18:40:18.747Z | 280.65° WNW | 17.97° | 2026-06-22 18:42:18.747Z | 247.063° WSW |
| 5 mins | 2026-06-23 05:17:18.747Z | 199.68° SSW | 2026-06-23 05:19:18.747Z | 263.433° W | 35.255° | 2026-06-23 05:22:18.747Z | 332.139° NNW |
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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