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: 13 hours ago
TLE from 13 hours ago
0 NETSAT-2
1 46507U 20068X 26004.53746000 .00023299 00000-0 61800-3 0 9998
2 46507 97.8612 359.9002 0003846 185.2990 174.8213 15.38318321290518Epoch: 2026-01-04T12:53Z
TLE epoch observation values (Epoch: 2026-01-04T12:53:56.543Z)
Latitude
-0.00012°
Longitude
62.26707°
Altitude
456.8 km
Speed
7.637 km/s
True Right ascension
23h 59m 36s
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
450.669 km
Perigee altitude
445.418 km
Semi-major axis
6,826.181 km
Eccentricity
0.00038
Inclination
97.8612°
RAAN
359.9002°
Arg. of periapsis
185.299°
True anomaly
174.82528°
Mean anomaly
174.8213°
Eccentric anomaly
174.82329°
Mean motion
3.84837 °/min
Orbital period
93.55 mins
BSTAR
0.000618
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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 | 2026-01-05 12:52:18.495Z | 352.546° N | 2026-01-05 12:55:18.495Z | 269.837° W | 30.727° | 2026-01-05 12:57:18.495Z | 223.755° SW |
| 5 mins | 2026-01-05 23:23:18.495Z | 147.699° SSE | 2026-01-05 23:25:18.495Z | 68.484° E | 40.386° | 2026-01-05 23:28:18.495Z | 356.331° N |
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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