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: 23 hours ago
TLE from 23 hours ago
0 NETSAT-2
1 46507U 20068X 25275.39804862 .00033733 00000-0 10380-2 0 9992
2 46507 97.8562 259.4553 0005799 157.9659 202.1832 15.33572824276065Epoch: 2025-10-02T09:33Z
TLE epoch observation values (Epoch: 2025-10-02T09:33:11.400Z)
Latitude
-0.00009°
Longitude
104.79853°
Altitude
471.934 km
Speed
7.628 km/s
True Right ascension
17h 17m 49s
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
02:10:26
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
466.097 km
Perigee altitude
458.164 km
Semi-major axis
6,840.268 km
Eccentricity
0.00058
Inclination
97.8562°
RAAN
259.4553°
Arg. of periapsis
157.9659°
True anomaly
202.15813°
Mean anomaly
202.1832°
Eccentric anomaly
202.17066°
Mean motion
3.83649 °/min
Orbital period
93.84 mins
BSTAR
0.001038
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-10-03 11:10:43.362Z | 46.883° ENE | 2025-10-03 11:13:43.362Z | 106.857° ESE | 18.417° | 2025-10-03 11:15:43.362Z | 143.339° SSE |
| 4 mins | 2025-10-03 12:44:43.362Z | 323.802° NNW | 2025-10-03 12:45:43.362Z | 302.178° NW | 18.831° | 2025-10-03 12:48:43.362Z | 241.726° WSW |
| 5 mins | 2025-10-03 23:16:43.362Z | 186.139° SSW | 2025-10-03 23:18:43.362Z | 279.692° WNW | 40.497° | 2025-10-03 23:21:43.362Z | 339.452° N |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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