GMS-T, 47346
Orbit data source: Space-Track
GMS-T, 47346 is a German payload satellite in LEO that was launched on Wed, 20 Jan 2021 UTC via an ELECTRON launch vehicle from the Rocket Lab Launch Complex (RLLC). 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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47346 intel report (Beta)
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Identifier
Orbit
Country
DE / GERRelated business
Manufacturer
OHB
Mission
Operational Commercial Communications
Bus & Motor
KLA, Unknown motor
Mass
50 kg wet, ~45 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 1 Pan, 1.5 m
Radar Cross Section
0.900 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 2 days ago
TLE from 2 days ago
0 GMS-T
1 47346U 21004A 26171.20326545 -.00000011 00000-0 -48850-4 0 9998
2 47346 90.1296 241.8667 0003935 61.4277 298.7250 13.16657488259990Epoch: 2026-06-20T04:52Z
TLE epoch observation values (Epoch: 2026-06-20T04:52:42.134Z)
Latitude
-0.00008°
Longitude
-99.73012°
Altitude
1,198.987 km
Speed
7.255 km/s
True Right ascension
16h 07m 28s
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
21:27:06
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,197.593 km
Perigee altitude
1,191.633 km
Semi-major axis
7,572.75 km
Eccentricity
0.00039
Inclination
90.1296°
RAAN
241.8667°
Arg. of periapsis
61.4277°
True anomaly
298.68545°
Mean anomaly
298.725°
Eccentric anomaly
298.70522°
Mean motion
3.29354 °/min
Orbital period
109.3 mins
BSTAR
-0.00004885
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Other satellites on launch #4 in the year 2021 (2021-01-20 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.GMS-T 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. |
|---|---|---|---|---|---|---|---|
| 11 mins | 2026-06-22 15:51:05.804Z | 24.911° NE | 2026-06-22 15:57:05.804Z | 85.791° E | 26.815° | 2026-06-22 16:02:05.804Z | 136.927° SSE |
| 11 mins | 2026-06-22 17:41:05.804Z | 344.698° N | 2026-06-22 17:46:05.804Z | 281.524° WNW | 36.242° | 2026-06-22 17:52:05.804Z | 212.059° SW |
| 11 mins | 2026-06-23 04:08:05.804Z | 138.365° SSE | 2026-06-23 04:13:05.804Z | 75.943° E | 33.439° | 2026-06-23 04:19:05.804Z | 13.473° NNE |
| 11 mins | 2026-06-23 05:57:05.804Z | 219.608° SW | 2026-06-23 06:02:05.804Z | 276.017° WNW | 29.611° | 2026-06-23 06:08:05.804Z | 337.983° 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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