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: 5 hours ago
TLE from 5 hours ago
0 SUPERVIEW NEO-1 03
1 63125U 25040A 26119.47263531 .00001334 00000-0 62137-4 0 9992
2 63125 97.3443 235.0411 0001704 84.6430 275.5001 15.21593051 64778Epoch: 2026-04-29T11:20Z
TLE epoch observation values (Epoch: 2026-04-29T11:20:35.690Z)
Latitude
0°
Longitude
-152.54071°
Altitude
504.017 km
Speed
7.612 km/s
True Right ascension
15h 40m 09s
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
23:40:34
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
499.168 km
Perigee altitude
496.824 km
Semi-major axis
6,876.133 km
Eccentricity
0.00017
Inclination
97.3443°
RAAN
235.0411°
Arg. of periapsis
84.643°
True anomaly
275.48066°
Mean anomaly
275.5001°
Eccentric anomaly
275.49038°
Mean motion
3.80651 °/min
Orbital period
94.57 mins
BSTAR
0.000062137
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-04-29 19:48:31.690Z | 45.019° ENE | 2026-04-29 19:51:31.690Z | 105.465° ESE | 20.835° | 2026-04-29 19:53:31.690Z | 143.212° SSE |
| 6 mins | 2026-04-30 07:59:31.690Z | 186.695° SSW | 2026-04-30 08:02:31.690Z | 289.413° WNW | 37.297° | 2026-04-30 08:05:31.690Z | 338.005° N |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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