Showing default

SUPERVIEW NEO 3-02, 63208

Orbit data source: Space-Track

SUPERVIEW NEO 3-02, 63208 is a payload satellite owned by Siwei (CN) in SSO that was launched on Sat, 15 Mar 2025 UTC via a CHANG ZHENG 2D 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
63208, 2025-051A
Orbit
SSO
Country
Flag of CNCN / PRC
Related business
Manufacturer
SAST
Mission
Operational Commercial Imaging
Bus & Motor
SIWEI, Unknown motor
Mass
~1,000 kg wet, ~700 kg dry
Launch date (UTC)
2025-03-15 (7 months ago)
Launch vehicle
CHANG ZHENG 2D
Launch site
Jiuquan Satellite Launch Center, China (JSC)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box, 3.0 m
Radar Cross Section
0.375 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 3 days ago

TLE from 3 days ago
0 SUPERVIEW NEO 3-02
1 63208U 25051A   25284.31807014  .00013846  00000-0  55811-3 0  9992
2 63208  97.4762   0.0308 0000546  55.5510 304.5780 15.24948803 31952
Epoch: 2025-10-11T07:38Z
TLE epoch observation values (Epoch: 2025-10-11T07:38:01.260Z)
Latitude
0.00008°
Longitude
-134.62574°
Altitude
493.821 km
Speed
7.618 km/s
True Right ascension
00h 00m 07s
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
00:31:27
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
488.276 km
Perigee altitude
487.527 km
Semi-major axis
6,866.038 km
Eccentricity
0.00005
Inclination
97.4762°
RAAN
0.0308°
Arg. of periapsis
55.551°
True anomaly
304.57285°
Mean anomaly
304.578°
Eccentric anomaly
304.57542°
Mean motion
3.81491 °/min
Orbital period
94.37 mins
BSTAR
0.00055811
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 #51 in the year 2025 (2025-03-15 UTC)

Documentation

Showing up to 5 results
|