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.
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46505 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: 19 hours ago
TLE from 19 hours ago
0 NETSAT-3
1 46505U 20068V 25257.52698465 .00011174 00000-0 37233-3 0 9997
2 46505 97.8551 239.7454 0004952 214.2521 145.8400 15.31282753273335Epoch: 2025-09-14T12:38Z
TLE epoch observation values (Epoch: 2025-09-14T12:38:51.473Z)
Latitude
-0.00006°
Longitude
56.28622°
Altitude
477.884 km
Speed
7.625 km/s
True Right ascension
15h 58m 58s
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
00:24:50
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
472.345 km
Perigee altitude
465.564 km
Semi-major axis
6,847.092 km
Eccentricity
0.0005
Inclination
97.8551°
RAAN
239.7454°
Arg. of periapsis
214.2521°
True anomaly
145.87185°
Mean anomaly
145.84°
Eccentric anomaly
145.85593°
Mean motion
3.83075 °/min
Orbital period
93.98 mins
BSTAR
0.00037233
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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-3 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-09-15 11:10:11.070Z | 39.529° NE | 2025-09-15 11:13:11.070Z | 101.027° ESE | 23.399° | 2025-09-15 11:15:11.070Z | 146.112° SSE |
| 5 mins | 2025-09-15 23:17:11.070Z | 195.324° SSW | 2025-09-15 23:19:11.070Z | 251.962° W | 34.703° | 2025-09-15 23:22:11.070Z | 331.097° NNW |
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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