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). Payloads include a variety of satellites, spacecraft, and rockets 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
S-NET A details
| Identifier | |
| Orbit | SSO |
| Last TLE update | 8 hours ago |
| Origin | |
| 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 | Payload Rocket body Debris |
| Shape & HBR | Box, 0.24 m |
| Radar Cross Section | 0.086 m², Medium (>0.1 m² and < 1m²) |
Expand to show TLE details & history
TLE from 8 hours ago
0 S-NET A
1 43188U 18014J 24361.27897634 .00011213 00000-0 71646-3 0 9995
2 43188 97.5777 260.1607 0012050 69.5872 290.6650 15.08745703377426Epoch: 2024-12-26T06:41Z
Definitive object data (Epoch: 2024-12-26T06:41:43.555Z)
| Latitude | 0.00001° |
| Longitude | 64.46856° |
| Altitude | 540.168 km |
| Speed | 7.594 km/s |
| True Right ascension | 17h 20m 38s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
| Latitude | -30.41354° |
| Longitude | 69.24463° |
| Altitude | 552.774 km |
| Speed | 7.583 km/s |
| Apparent Right ascension | 21h 04m 32s |
| Apparent Declination | -55° 12' 33" |
| Sunlit | Object is in daylight |
Visualization observer readout
| Local Sidereal Time | 13:52:59 |
| Azimuth | 133.618° SE |
| Elevation | -41.405° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 545.353 km |
| Perigee altitude | 528.687 km |
| Semi-major axis | 6,915.157 km |
| Eccentricity | 0.001205 |
| Inclination | 97.5777° |
| RAAN | 260.1607° |
| Arg. of periapsis | 69.5872° |
| True anomaly | 290.53573° |
| Mean anomaly | 290.665° |
| Eccentric anomaly | 290.60037° |
| Mean motion | 3.77433 °/min |
| BSTAR | 0.00071646 |
| Orbital period | 95.38 mins |
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Other satellites on launch #14 in the year 2018 (2018-02-01 UTC)
| KANOPUS-V 3, 43180 |
| KANOPUS-V 4, 43181 |
| LEMUR 2 JIN-LUEN, 43182 |
| LEMUR 2 URAMCHANSOL, 43183 |
| LEMUR 2 KADI, 43184 |
| LEMUR 2 THENICKMOLO, 43185 |
| S-NET D, 43186 |
| S-NET B, 43187 |
| S-NET A, 43188 |
| S-NET C, 43189 |
S-NET A Visibility forecast
Observer location: undefined°, undefined
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 | 2024-12-26 17:58:08.179Z | 198.128° SSW | 2024-12-26 18:01:08.179Z | 281.746° WNW | 31.832° | 2024-12-26 18:04:08.179Z | 331.789° NNW |
| 4 mins | 2024-12-27 05:34:08.179Z | 56.075° ENE | 2024-12-27 05:36:08.179Z | 95.684° ESE | 20.062° | 2024-12-27 05:38:08.179Z | 134.729° SE |
| 4 mins | 2024-12-27 07:09:08.179Z | 323.269° NNW | 2024-12-27 07:10:08.179Z | 301.311° NW | 22.243° | 2024-12-27 07:13:08.179Z | 240.571° WSW |
Authenticating...
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