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.
Focus sentinelFocus sentinel
Request partner network tasking
Focus sentinelFocus sentinel
Embed this page
Focus sentinelFocus sentinel
63126 intel report (Beta)
Focus sentinelFocus sentinel
Create New Watchlist
Focus sentinelFocus sentinel
Edit Public Description
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: 3 days ago
TLE from 3 days ago
0 SUPERVIEW NEO-1 04
1 63126U 25040B 25346.70094303 -.00000491 00000-0 -18791-4 0 9991
2 63126 97.3396 100.7197 0001648 94.5806 265.5618 15.21657901 43831Epoch: 2025-12-12T16:49Z
TLE epoch observation values (Epoch: 2025-12-12T16:49:21.477Z)
Latitude
-0.00009°
Longitude
126.74143°
Altitude
504.022 km
Speed
7.612 km/s
True Right ascension
06h 42m 52s
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
13:24:48
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
498.933 km
Perigee altitude
496.667 km
Semi-major axis
6,875.937 km
Eccentricity
0.00016
Inclination
97.3396°
RAAN
100.7197°
Arg. of periapsis
94.5806°
True anomaly
265.54297°
Mean anomaly
265.5618°
Eccentric anomaly
265.55239°
Mean motion
3.80667 °/min
Orbital period
94.57 mins
BSTAR
-0.000018791
Loading maneuver chart data...
Computing Atmospheric mass density...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Other satellites on launch #40 in the year 2025 (2025-02-27 UTC)
Did you know?
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 | 2025-12-15 21:09:13.612Z | 338.027° N | 2025-12-15 21:11:13.612Z | 278.618° WNW | 29.676° | 2025-12-15 21:14:13.612Z | 221.469° SW |
| 5 mins | 2025-12-16 07:46:13.612Z | 161.207° S | 2025-12-16 07:48:13.612Z | 57.894° ENE | 44.531° | 2025-12-16 07:51:13.612Z | 350.967° 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 |
|---|
CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
Authenticating...
Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in descending order |
|---|