SUPERVIEW NEO 3-02, 63208
Orbit data source: Space-Track
SUPERVIEW NEO 3-02, 63208 is a payload satellite owned by Siwei (CN) in SSO that was launched on Sat, 15 Mar 2025 UTC via a CHANG ZHENG 2D 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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63208 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
SAST
Mission
Operational Commercial Imaging
Bus & Motor
SIWEI, Unknown motor
Mass
~1,000 kg wet, ~700 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 3.0 m
Radar Cross Section
0.375 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 9 hours ago
TLE from 9 hours ago
0 SUPERVIEW NEO 3-02
1 63208U 25051A 25312.51949434 .00016350 00000-0 70492-3 0 9994
2 63208 97.4740 28.0639 0001385 150.1129 210.0187 15.22633568 36241Epoch: 2025-11-08T12:28Z
TLE epoch observation values (Epoch: 2025-11-08T12:28:04.310Z)
Latitude
-0.00002°
Longitude
153.09801°
Altitude
501.817 km
Speed
7.613 km/s
True Right ascension
01h 52m 15s
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
17:26:25
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
495.818 km
Perigee altitude
493.914 km
Semi-major axis
6,873.003 km
Eccentricity
0.00014
Inclination
97.474°
RAAN
28.0639°
Arg. of periapsis
150.1129°
True anomaly
210.01076°
Mean anomaly
210.0187°
Eccentric anomaly
210.01473°
Mean motion
3.80911 °/min
Orbital period
94.51 mins
BSTAR
0.00070492
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Other satellites on launch #51 in the year 2025 (2025-03-15 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 3-02 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 | 2025-11-09 04:23:40.098Z | 109.238° ESE | 2025-11-09 04:25:40.098Z | 69.859° E | 18.962° | 2025-11-09 04:27:40.098Z | 30.015° NE |
| 4 mins | 2025-11-09 05:57:40.098Z | 227.673° WSW | 2025-11-09 05:59:40.098Z | 275.228° WNW | 21.213° | 2025-11-09 06:01:40.098Z | 313.078° NW |
| 4 mins | 2025-11-09 17:26:40.098Z | 52.624° ENE | 2025-11-09 17:28:40.098Z | 103.271° ESE | 24.515° | 2025-11-09 17:30:40.098Z | 147.003° SSE |
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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