Showing default

SUPERVIEW NEO-2 03, 62079

Orbit data source: Space-Track

SUPERVIEW NEO-2 03, 62079 is a payload satellite owned by Siwei (CN) in SSO that was launched on Sun, 24 Nov 2024 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
62079, 2024-218B
Orbit
SSO
Country
Flag of CNCN / PRC
Related business
Manufacturer
DFH
Mission
Operational Commercial Radar Imaging
Bus & Motor
SIWEI, Unknown motor
Mass
600 kg wet, ~500 kg dry
Launch date (UTC)
2024-11-24 (1 year 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
Last TLE update: 1 day ago

TLE from 1 day ago
0 SUPERVIEW NEO-2 03
1 62079U 24218B   26135.39320626  .00000045  00000-0  52852-5 0  9995
2 62079  97.4395 143.1896 0001625  88.1372 272.0049 15.19715568 81469
Epoch: 2026-05-15T09:26Z
TLE epoch observation values (Epoch: 2026-05-15T09:26:13.020Z)
Latitude
-0.00005°
Longitude
128.51019°
Altitude
509.75 km
Speed
7.609 km/s
True Right ascension
09h 32m 45s
True Declination
0° 00' 00"
Sunlit
Object was in daylight 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
20:51:20
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
504.785 km
Perigee altitude
502.549 km
Semi-major axis
6,881.804 km
Eccentricity
0.00016
Inclination
97.4395°
RAAN
143.1896°
Arg. of periapsis
88.1372°
True anomaly
271.98629°
Mean anomaly
272.0049°
Eccentric anomaly
271.9956°
Mean motion
3.8018 °/min
Orbital period
94.69 mins
BSTAR
0.0000052852
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 #218 in the year 2024 (2024-11-24 UTC)

Documentation

Showing up to 5 results
|