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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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: 12 hours ago
TLE from 12 hours ago
0 NETSAT-2
1 46507U 20068X 26053.22096019 .00025590 00000-0 62699-3 0 9999
2 46507 97.8656 52.1478 0006600 60.9249 299.2656 15.40713673298009Epoch: 2026-02-22T05:18Z
TLE epoch observation values (Epoch: 2026-02-22T05:18:10.960Z)
Latitude
-0.00004°
Longitude
-179.53017°
Altitude
444.907 km
Speed
7.646 km/s
True Right ascension
03h 28m 35s
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
20:54:51
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
445.461 km
Perigee altitude
436.46 km
Semi-major axis
6,819.098 km
Eccentricity
0.00066
Inclination
97.8656°
RAAN
52.1478°
Arg. of periapsis
60.9249°
True anomaly
299.1996°
Mean anomaly
299.2656°
Eccentric anomaly
299.2326°
Mean motion
3.85436 °/min
Orbital period
93.4 mins
BSTAR
0.00062699
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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 | 2026-02-23 00:07:45.775Z | 184.009° SSW | 2026-02-23 00:10:45.775Z | 262.201° W | 37.176° | 2026-02-23 00:13:45.775Z | 335.502° NNW |
| 5 mins | 2026-02-23 13:02:45.775Z | 351.41° N | 2026-02-23 13:04:45.775Z | 274.602° WNW | 36.615° | 2026-02-23 13:07:45.775Z | 210.651° 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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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