Showing default

SUPERVIEW NEO-1 03, 63125

Orbit data source: Space-Track

SUPERVIEW NEO-1 03, 63125 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
63125, 2025-040A
Orbit
SSO
Last TLE update
2 days 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 2 days ago
0 SUPERVIEW NEO-1 03
1 63125U 25040A   25234.90805156  .00008053  00000-0  35943-3 0  9991
2 63125  97.3304 351.7136 0001880 114.5916 245.5517 15.21630617 26824
Epoch: 2025-08-22T21:47Z
TLE epoch observation values (Epoch: 2025-08-22T21:47:35.654Z)
Latitude
0.00003°
Longitude
53.36461°
Altitude
504.552 km
Speed
7.612 km/s
True Right ascension
23h 26m 51s
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
11:12:30
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
499.175 km
Perigee altitude
496.589 km
Semi-major axis
6,876.019 km
Eccentricity
0.00019
Inclination
97.3304°
RAAN
351.7136°
Arg. of periapsis
114.5916°
True anomaly
245.53209°
Mean anomaly
245.5517°
Eccentric anomaly
245.54189°
Mean motion
3.8066 °/min
Orbital period
94.57 mins
BSTAR
0.00035943
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
|