Showing default

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.

Loading next visibility...
Identifier
63126, 2025-040B
Orbit
SSO
Country
Flag of CNCN / PRC
Related business
Manufacturer
SAST
Mission
Operational Commercial Imaging
Bus & Motor
SIWEI, Unknown motor
Mass
540 kg wet, ~500 kg dry
Launch date (UTC)
2025-02-27 (2 years ago)
Launch vehicle
CHANG ZHENG 2C
Launch site
Jiuquan Satellite Launch Center, China (JSC)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box, 4.4 m
Radar Cross Section
0.375 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 6 hours ago

TLE from 6 hours ago
0 SUPERVIEW NEO-1 04
1 63126U 25040B   26249.61584142  .00005036  00000-0  22595-3 0  9993
2 63126  97.3579   2.2857 0001673  51.9119 308.2268 15.21635035 84571
Epoch: 2026-09-06T14:46Z
TLE epoch observation values (Epoch: 2026-09-06T14:46:48.698Z)
Latitude
-0.00002°
Longitude
154.87439°
Altitude
503.29 km
Speed
7.613 km/s
True Right ascension
00h 09m 08s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
12:54:18
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
499.02 km
Perigee altitude
496.72 km
Semi-major axis
6,876.007 km
Eccentricity
0.00017
Inclination
97.3579°
RAAN
2.2857°
Arg. of periapsis
51.9119°
True anomaly
308.21174°
Mean anomaly
308.2268°
Eccentric anomaly
308.21927°
Mean motion
3.80661 °/min
Orbital period
94.57 mins
BSTAR
0.00022595
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)

Documentation

Showing up to 5 results
|