SUPERVIEW NEO-1 03, 63125
Orbit data source: Space-Track
SUPERVIEW NEO-1 03, 63125 is a payload satellite owned by Siwei (CN) in SSO that was launched on Thu, 27 Feb 2025 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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63125 intel report (Beta)
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Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
SAST
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, 4.7 m
Radar Cross Section
0.375 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 8 hours ago
TLE from 8 hours ago
0 SUPERVIEW NEO-1 03
1 63125U 25040A 26220.94286288 .00001322 00000-0 61551-4 0 9997
2 63125 97.3538 334.1406 0001855 84.9118 275.2330 15.21621078 80200Epoch: 2026-08-08T22:37Z
TLE epoch observation values (Epoch: 2026-08-08T22:37:43.352Z)
Latitude
-0.00003°
Longitude
37.26301°
Altitude
503.928 km
Speed
7.612 km/s
True Right ascension
22h 16m 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
20:20:12
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
499.187 km
Perigee altitude
496.636 km
Semi-major axis
6,876.049 km
Eccentricity
0.00019
Inclination
97.3538°
RAAN
334.1406°
Arg. of periapsis
84.9118°
True anomaly
275.21183°
Mean anomaly
275.233°
Eccentric anomaly
275.22242°
Mean motion
3.80658 °/min
Orbital period
94.57 mins
BSTAR
0.000061551
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Other satellites on launch #40 in the year 2025 (2025-02-27 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 03 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 | 2026-08-09 06:40:39.443Z | 102.865° ESE | 2026-08-09 06:42:39.443Z | 68.077° E | 15.135° | 2026-08-09 06:44:39.443Z | 33.104° NE |
| 4 mins | 2026-08-09 08:14:39.443Z | 220.227° SW | 2026-08-09 08:16:39.443Z | 278.781° WNW | 26.316° | 2026-08-09 08:18:39.443Z | 319.428° NNW |
| 4 mins | 2026-08-09 19:44:39.443Z | 67.786° E | 2026-08-09 19:45:39.443Z | 90.706° ESE | 20.283° | 2026-08-09 19:48:39.443Z | 146.783° 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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