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: 14 hours ago
TLE from 14 hours ago
0 NETSAT-1
1 46506U 20068W 26004.49910675 .00016659 00000-0 57840-3 0 9994
2 46506 97.8680 354.9138 0004761 199.8289 160.2766 15.29845966290237Epoch: 2026-01-04T11:58Z
TLE epoch observation values (Epoch: 2026-01-04T11:58:42.823Z)
Latitude
0.00002°
Longitude
71.12562°
Altitude
482.435 km
Speed
7.622 km/s
True Right ascension
23h 39m 39s
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
02:04:35
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
476.507 km
Perigee altitude
469.984 km
Semi-major axis
6,851.383 km
Eccentricity
0.00048
Inclination
97.868°
RAAN
354.9138°
Arg. of periapsis
199.8289°
True anomaly
160.295°
Mean anomaly
160.2766°
Eccentric anomaly
160.2858°
Mean motion
3.82715 °/min
Orbital period
94.06 mins
BSTAR
0.0005784
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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 | 2026-01-05 12:05:18.707Z | 14.679° NNE | 2026-01-05 12:08:18.707Z | 168.587° S | 43.898° | 2026-01-05 12:11:18.707Z | 191.118° SSW |
| 4 mins | 2026-01-05 22:40:18.707Z | 112.475° ESE | 2026-01-05 22:42:18.707Z | 55.652° ENE | 24.73° | 2026-01-05 22:44:18.707Z | 16.083° NNE |
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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