NETSAT-1, 46506
Orbit data source: Space-Track
NETSAT-1, 46506 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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46506 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-1
1 46506U 20068W 25322.51097258 .00016933 00000-0 61734-3 0 9994
2 46506 97.8649 305.2602 0007612 40.8389 319.3419 15.28226411283052Epoch: 2025-11-18T12:15Z
TLE epoch observation values (Epoch: 2025-11-18T12:15:48.030Z)
Latitude
0.00001°
Longitude
63.51406°
Altitude
480.242 km
Speed
7.628 km/s
True Right ascension
20h 21m 02s
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
18:06:38
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
483.308 km
Perigee altitude
472.87 km
Semi-major axis
6,856.226 km
Eccentricity
0.00076
Inclination
97.8649°
RAAN
305.2602°
Arg. of periapsis
40.8389°
True anomaly
319.28503°
Mean anomaly
319.3419°
Eccentric anomaly
319.31347°
Mean motion
3.8231 °/min
Orbital period
94.16 mins
BSTAR
0.00061734
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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-1 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 22:57:31.246Z | 162.717° S | 2025-11-19 23:00:31.246Z | 111.341° ESE | 44.388° | 2025-11-19 23:03:31.246Z | 350.314° N |
| 5 mins | 2025-11-20 11:58:31.246Z | 9.051° NNE | 2025-11-20 12:00:31.246Z | 342.804° N | 43.643° | 2025-11-20 12:03:31.246Z | 197.529° 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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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