SUPERVIEW NEO-2 02, 53130
Orbit data source: Space-Track
SUPERVIEW NEO-2 02, 53130 is a payload satellite owned by Siwei (CN) in SSO that was launched on Fri, 15 Jul 2022 UTC via a CHANG ZHENG 2C launch vehicle from the Taiyaun Space Center, China (TSC). 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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53130 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, 0.3 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 02
1 53130U 22082C 26171.14562491 .00000927 00000-0 40591-4 0 9996
2 53130 97.3939 181.1191 0001682 89.0807 271.0623 15.24506744218667Epoch: 2026-06-20T03:29Z
TLE epoch observation values (Epoch: 2026-06-20T03:29:41.992Z)
Latitude
-0.00004°
Longitude
-139.67031°
Altitude
495.343 km
Speed
7.617 km/s
True Right ascension
12h 04m 28s
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
21:32:28
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
490.381 km
Perigee altitude
488.071 km
Semi-major axis
6,867.363 km
Eccentricity
0.00017
Inclination
97.3939°
RAAN
181.1191°
Arg. of periapsis
89.0807°
True anomaly
271.04303°
Mean anomaly
271.0623°
Eccentric anomaly
271.05266°
Mean motion
3.8138 °/min
Orbital period
94.39 mins
BSTAR
0.000040591
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Other satellites on launch #82 in the year 2022 (2022-07-15 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 02 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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-06-22 12:47:26.680Z | 55.97° ENE | 2026-06-22 12:49:26.680Z | 98.233° ESE | 19.559° | 2026-06-22 12:51:26.680Z | 137.888° SSE |
| 4 mins | 2026-06-22 14:21:26.680Z | 321.467° NNW | 2026-06-22 14:22:26.680Z | 299.435° NW | 20.084° | 2026-06-22 14:25:26.680Z | 240.454° WSW |
| 5 mins | 2026-06-23 00:56:26.680Z | 182.9° SSW | 2026-06-23 00:58:26.680Z | 223.246° SW | 39.148° | 2026-06-23 01:01:26.680Z | 336.711° 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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