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: 16 hours ago
TLE from 16 hours ago
0 SUPERVIEW NEO-1 04
1 63126U 25040B 26118.94703429 .00008861 00000-0 39482-3 0 9997
2 63126 97.3463 234.6133 0002813 99.6222 260.5332 15.21656351 64701Epoch: 2026-04-28T22:43Z
TLE epoch observation values (Epoch: 2026-04-28T22:43:43.762Z)
Latitude
-0.00004°
Longitude
36.76592°
Altitude
504.257 km
Speed
7.612 km/s
True Right ascension
15h 38m 27s
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
22:28:56
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
499.739 km
Perigee altitude
495.871 km
Semi-major axis
6,875.942 km
Eccentricity
0.00028
Inclination
97.3463°
RAAN
234.6133°
Arg. of periapsis
99.6222°
True anomaly
260.50141°
Mean anomaly
260.5332°
Eccentric anomaly
260.5173°
Mean motion
3.80667 °/min
Orbital period
94.57 mins
BSTAR
0.00039482
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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
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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-04-29 19:49:04.812Z | 43.729° NE | 2026-04-29 19:52:04.812Z | 102.928° ESE | 21.104° | 2026-04-29 19:54:04.812Z | 142.165° SSE |
| 4 mins | 2026-04-29 21:24:04.812Z | 319.99° NNW | 2026-04-29 21:25:04.812Z | 298.89° NW | 19.025° | 2026-04-29 21:28:04.812Z | 242.513° WSW |
| 5 mins | 2026-04-30 08:01:04.812Z | 196.065° SSW | 2026-04-30 08:03:04.812Z | 285.12° WNW | 37.535° | 2026-04-30 08:06:04.812Z | 337.554° N |
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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