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: 1 day ago
TLE from 1 day ago
0 NETSAT-3
1 46505U 20068V 25338.78732736 .00033863 00000-0 99809-3 0 9991
2 46505 97.8609 326.0751 0005046 330.1567 29.9386 15.34941614285780Epoch: 2025-12-04T18:53Z
TLE epoch observation values (Epoch: 2025-12-04T18:53:45.083Z)
Latitude
-0.0001°
Longitude
-31.20149°
Altitude
461.2 km
Speed
7.638 km/s
True Right ascension
21h 44m 18s
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
17:52:58
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
461.51 km
Perigee altitude
454.61 km
Semi-major axis
6,836.197 km
Eccentricity
0.0005
Inclination
97.8609°
RAAN
326.0751°
Arg. of periapsis
330.1567°
True anomaly
29.96747°
Mean anomaly
29.9386°
Eccentric anomaly
29.95304°
Mean motion
3.83991 °/min
Orbital period
93.75 mins
BSTAR
0.00099809
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-12-05 23:10:58.904Z | 156.781° SSE | 2025-12-05 23:13:58.904Z | 84.154° E | 42.243° | 2025-12-05 23:16:58.904Z | 354.602° N |
| 5 mins | 2025-12-06 12:08:58.904Z | 20.167° NNE | 2025-12-06 12:10:58.904Z | 128.719° SE | 43.732° | 2025-12-06 12:13:58.904Z | 187.727° SSW |
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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