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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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Identifier
63126, 2025-040B
Orbit
SSO
Last TLE update
21 hours ago
Origin
Manufacturer
SAST
Mission
Operational Commercial Imaging
Bus & Motor
SIWEI, Unknown motor
Mass
540 kg wet, ~500 kg dry
Launch date (UTC)
2025-02-27 (6 months ago)
Launch vehicle
CHANG ZHENG 2C
Launch site
Jiuquan Satellite Launch Center, China (JSC)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box, 0.3 m
Radar Cross Section
0.375 m², Large (>1 m²)

Expand to show TLE details & history

TLE from 21 hours ago
0 SUPERVIEW NEO-1 04
1 63126U 25040B   25235.96091110  .00007530  00000-0  33652-3 0  9990
2 63126  97.3316 352.7595 0001915 110.8518 249.2924 15.21609229 26990
Epoch: 2025-08-23T23:03Z
TLE epoch observation values (Epoch: 2025-08-23T23:03:42.719Z)
Latitude
0.00006°
Longitude
34.34332°
Altitude
504.547 km
Speed
7.612 km/s
True Right ascension
23h 31m 02s
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
10:59:15
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
499.263 km
Perigee altitude
496.63 km
Semi-major axis
6,876.084 km
Eccentricity
0.00019
Inclination
97.3316°
RAAN
352.7595°
Arg. of periapsis
110.8518°
True anomaly
249.27188°
Mean anomaly
249.2924°
Eccentric anomaly
249.28214°
Mean motion
3.80655 °/min
Orbital period
94.57 mins
BSTAR
0.00033652
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Other satellites on launch #40 in the year 2025 (2025-02-27 UTC)

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