SUPERVIEW NEO-1 04, 63126
Orbit data source: Space-Track
SUPERVIEW NEO-1 04, 63126 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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63126 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, 4.4 m
Radar Cross Section
0.375 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 SUPERVIEW NEO-1 04
1 63126U 25040B 26219.95703458 -.00000534 00000-0 -20667-4 0 9999
2 63126 97.3559 333.2948 0002822 98.1104 262.0452 15.21632820 80062Epoch: 2026-08-07T22:58Z
TLE epoch observation values (Epoch: 2026-08-07T22:58:07.787Z)
Latitude
-0.00008°
Longitude
32.28708°
Altitude
504.278 km
Speed
7.612 km/s
True Right ascension
22h 13m 10s
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
19:20:49
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
499.817 km
Perigee altitude
495.936 km
Semi-major axis
6,876.014 km
Eccentricity
0.00028
Inclination
97.3559°
RAAN
333.2948°
Arg. of periapsis
98.1104°
True anomaly
262.01317°
Mean anomaly
262.0452°
Eccentric anomaly
262.02919°
Mean motion
3.80661 °/min
Orbital period
94.57 mins
BSTAR
-0.000020667
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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 04 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 06:41:25.821Z | 103.918° ESE | 2026-08-09 06:43:25.821Z | 69.387° E | 15.253° | 2026-08-09 06:45:25.821Z | 33.855° NE |
| 4 mins | 2026-08-09 08:15:25.821Z | 219.365° SW | 2026-08-09 08:17:25.821Z | 276.561° WNW | 26.289° | 2026-08-09 08:19:25.821Z | 318.44° NNW |
| 4 mins | 2026-08-09 19:45:25.821Z | 66.494° ENE | 2026-08-09 19:46:25.821Z | 89.259° E | 20.379° | 2026-08-09 19:49:25.821Z | 146.452° 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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