Showing default

NETSAT-3, 46505

Orbit data source: Space-Track

NETSAT-3, 46505 is a payload satellite owned by ZfT (DE) in SSO that was launched on Mon, 28 Sep 2020 UTC via a SOYUZ-2-1B launch vehicle from the Plesetsk Missile And Space Complex (PKMTR). 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
46505, 2020-068V
Orbit
SSO
Country
Flag of DEDE / GER
Related business
Manufacturer
ZfT
Mission
Operational Commercial Technology
Bus & Motor
CUBESAT 3U, Unknown motor
Mass
4 kg wet, 4 kg dry
Launch date (UTC)
2020-09-28 (5 years ago)
Launch vehicle
SOYUZ-2-1B
Launch site
Plesetsk Missile And Space Complex (PKMTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box, Unknown HBR
Radar Cross Section
0.035 m², Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 19 hours ago

TLE from 19 hours ago
0 NETSAT-3
1 46505U 20068V   25287.90027758  .00019260  00000-0  61237-3 0  9998
2 46505  97.8591 271.9507 0008842 117.2113 243.0030 15.32629854277980
Epoch: 2025-10-14T21:36Z
TLE epoch observation values (Epoch: 2025-10-14T21:36:23.982Z)
Latitude
-0.00002°
Longitude
-75.83129°
Altitude
473.816 km
Speed
7.627 km/s
True Right ascension
18h 07m 48s
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
11:07:28
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
470.989 km
Perigee altitude
458.888 km
Semi-major axis
6,843.076 km
Eccentricity
0.00088
Inclination
97.8591°
RAAN
271.9507°
Arg. of periapsis
117.2113°
True anomaly
242.91276°
Mean anomaly
243.003°
Eccentric anomaly
242.95788°
Mean motion
3.83412 °/min
Orbital period
93.89 mins
BSTAR
0.00061237
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...

Documentation

Showing up to 5 results
|