NETSAT-2, 46507
Orbit data source: Space-Track
NETSAT-2, 46507 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.
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46507 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
DE / GERRelated business
Manufacturer
ZfT
Mission
Operational Commercial Technology
Bus & Motor
CUBESAT 3U, Unknown motor
Mass
4 kg wet, 4 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, Unknown HBR
Radar Cross Section
0.035 m², Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 NETSAT-2
1 46507U 20068X 25322.47178803 .00023119 00000-0 66010-3 0 9992
2 46507 97.8586 309.5879 0006653 43.6574 316.5193 15.36014435283280Epoch: 2025-11-18T11:19Z
TLE epoch observation values (Epoch: 2025-11-18T11:19:22.485Z)
Latitude
-0.00012°
Longitude
81.98684°
Altitude
457.708 km
Speed
7.64 km/s
True Right ascension
20h 38m 21s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
18:09:22
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
459.42 km
Perigee altitude
450.328 km
Semi-major axis
6,833.011 km
Eccentricity
0.00067
Inclination
97.8586°
RAAN
309.5879°
Arg. of periapsis
43.6574°
True anomaly
316.46681°
Mean anomaly
316.5193°
Eccentric anomaly
316.49306°
Mean motion
3.8426 °/min
Orbital period
93.69 mins
BSTAR
0.0006601
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Other satellites on launch #68 in the year 2020 (2020-09-28 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.NETSAT-2 Visibility forecast
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-11-19 23:24:14.750Z | 172.257° S | 2025-11-19 23:27:14.750Z | 236.612° WSW | 43.804° | 2025-11-19 23:30:14.750Z | 343.075° N |
| 5 mins | 2025-11-20 12:21:14.750Z | 3.919° NNE | 2025-11-20 12:23:14.750Z | 323.314° NNW | 41.22° | 2025-11-20 12:26:14.750Z | 203.725° SW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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