S-NET A, 43188
Orbit data source: Space-Track
S-NET A, 43188 is a payload satellite owned by TUB (DE) in SSO that was launched on Thu, 01 Feb 2018 UTC via a SOYUZ-2-1A launch vehicle from the Vostochny Cosmodrome (VOSTO). 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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43188 intel report (Beta)
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S-NET A radio frequencies
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Edit Public Description
Identifier
Orbit
Country
DE / GERRelated business
Manufacturer
TUB
Mission
Operational Commercial Com/Tech
Bus & Motor
TUBIX10, Unknown motor
Mass
8 kg wet, 8 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 0.1 m
Radar Cross Section
0.086 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 S-NET A
1 43188U 18014J 25259.68549629 .00006184 00000-0 35593-3 0 9997
2 43188 97.5514 161.7181 0007832 233.6889 126.3620 15.12778013417356Epoch: 2025-09-16T16:27Z
TLE epoch observation values (Epoch: 2025-09-16T16:27:06.879Z)
Latitude
0.00006°
Longitude
-80.93282°
Altitude
534.019 km
Speed
7.594 km/s
True Right ascension
10h 46m 52s
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
17:05:27
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
530.121 km
Perigee altitude
519.308 km
Semi-major axis
6,902.851 km
Eccentricity
0.00078
Inclination
97.5514°
RAAN
161.7181°
Arg. of periapsis
233.6889°
True anomaly
126.43423°
Mean anomaly
126.362°
Eccentric anomaly
126.39812°
Mean motion
3.78443 °/min
Orbital period
95.13 mins
BSTAR
0.00035593
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Other satellites on launch #14 in the year 2018 (2018-02-01 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.S-NET A 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 | 2025-09-18 05:33:13.137Z | 57.498° ENE | 2025-09-18 05:35:13.137Z | 94.507° ESE | 17.686° | 2025-09-18 05:37:13.137Z | 131.308° SE |
| 4 mins | 2025-09-18 07:08:13.137Z | 322.071° NNW | 2025-09-18 07:09:13.137Z | 296.981° NW | 24.575° | 2025-09-18 07:12:13.137Z | 234.854° WSW |
| 5 mins | 2025-09-18 17:48:13.137Z | 184.245° SSW | 2025-09-18 17:50:13.137Z | 246.398° WSW | 41.499° | 2025-09-18 17:53:13.137Z | 338.137° 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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