SUPERVIEW NEO-1 02, 52322
Orbit data source: Space-Track
SUPERVIEW NEO-1 02, 52322 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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52322 intel report (Beta)
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Edit Public Description
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: 16 hours ago
TLE from 16 hours ago
0 SUPERVIEW NEO-1 02
1 52322U 22043C 25348.96210333 .00004865 00000-0 26882-3 0 9996
2 52322 97.3622 62.7507 0000556 205.5183 154.6022 15.14354687201672Epoch: 2025-12-14T23:05Z
TLE epoch observation values (Epoch: 2025-12-14T23:05:25.727Z)
Latitude
-0.00002°
Longitude
-7.47399°
Altitude
526.369 km
Speed
7.6 km/s
True Right ascension
04h 11m 00s
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
13:24:44
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
520.293 km
Perigee altitude
519.526 km
Semi-major axis
6,898.047 km
Eccentricity
0.00006
Inclination
97.3622°
RAAN
62.7507°
Arg. of periapsis
205.5183°
True anomaly
154.60493°
Mean anomaly
154.6022°
Eccentric anomaly
154.60357°
Mean motion
3.78838 °/min
Orbital period
95.03 mins
BSTAR
0.00026882
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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 02 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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2025-12-15 17:07:09.822Z | 53.396° ENE | 2025-12-15 17:09:09.822Z | 90.094° ESE | 18.641° | 2025-12-15 17:11:09.822Z | 129.908° SE |
| 4 mins | 2025-12-15 18:42:09.822Z | 322.54° NNW | 2025-12-15 18:43:09.822Z | 299.266° NW | 22.908° | 2025-12-15 18:46:09.822Z | 237.718° WSW |
| 6 mins | 2025-12-16 05:21:09.822Z | 182.534° SSW | 2025-12-16 05:24:09.822Z | 291.091° WNW | 39.903° | 2025-12-16 05:27:09.822Z | 339.786° N |
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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