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: 5 hours ago
TLE from 5 hours ago
0 SUPERVIEW NEO-1 04
1 63126U 25040B 26164.84834807 .00009435 00000-0 42090-3 0 9999
2 63126 97.3525 279.4439 0000215 76.8853 283.2407 15.21600884 71687Epoch: 2026-06-13T20:21Z
TLE epoch observation values (Epoch: 2026-06-13T20:21:37.273Z)
Latitude
-0.00002°
Longitude
71.88105°
Altitude
504.071 km
Speed
7.612 km/s
True Right ascension
18h 37m 46s
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
11:53:05
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
498.121 km
Perigee altitude
497.825 km
Semi-major axis
6,876.11 km
Eccentricity
0.00002
Inclination
97.3525°
RAAN
279.4439°
Arg. of periapsis
76.8853°
True anomaly
283.2383°
Mean anomaly
283.2407°
Eccentric anomaly
283.2395°
Mean motion
3.80653 °/min
Orbital period
94.57 mins
BSTAR
0.0004209
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-06-14 07:32:05.966Z | 156.944° SSE | 2026-06-14 07:35:05.966Z | 86.507° E | 42.382° | 2026-06-14 07:38:05.966Z | 355.703° N |
| 5 mins | 2026-06-14 20:37:05.966Z | 5.314° NNE | 2026-06-14 20:39:05.966Z | 224.466° SW | 42.994° | 2026-06-14 20:42:05.966Z | 197.269° SSW |
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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