NETSAT-4, 46504
Orbit data source: Space-Track
NETSAT-4, 46504 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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46504 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: 14 hours ago
TLE from 14 hours ago
0 NETSAT-4
1 46504U 20068U 26020.22662767 .00027896 00000-0 74136-3 0 9999
2 46504 97.8611 17.1938 0008129 118.2173 241.9893 15.38194815292986Epoch: 2026-01-20T05:26Z
TLE epoch observation values (Epoch: 2026-01-20T05:26:20.630Z)
Latitude
0.00002°
Longitude
175.9963°
Altitude
457.16 km
Speed
7.637 km/s
True Right ascension
01h 08m 46s
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
20:54:04
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
453.959 km
Perigee altitude
442.86 km
Semi-major axis
6,826.546 km
Eccentricity
0.00081
Inclination
97.8611°
RAAN
17.1938°
Arg. of periapsis
118.2173°
True anomaly
241.9071°
Mean anomaly
241.9893°
Eccentric anomaly
241.9482°
Mean motion
3.84806 °/min
Orbital period
93.55 mins
BSTAR
0.00074136
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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-4 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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-01-21 00:18:43.717Z | 215.561° SW | 2026-01-21 00:20:43.717Z | 266.832° W | 23.827° | 2026-01-21 00:22:43.717Z | 313.453° NW |
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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