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 | 15 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 15 hours ago
0 S-NET A
1 43188U 18014J 24346.28876659 .00009009 00000-0 58099-3 0 9990
2 43188 97.5770 245.3662 0011885 113.8702 246.3773 15.08469543375163Epoch: 2024-12-11T06:55Z
Definitive object data (Epoch: 2024-12-11T06:55:49.433Z)
| Latitude | -0.00003° |
| Longitude | 60.92464° |
| Altitude | 547.25 km |
| Speed | 7.587 km/s |
| True Right ascension | 16h 21m 27s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
| Latitude | 78.64035° |
| Longitude | 20.34409° |
| Altitude | 546.974 km |
| Speed | 7.599 km/s |
| Apparent Right ascension | 09h 01m 34s |
| Apparent Declination | 27° 22' 04" |
| Sunlit | Object is in daylight |
Visualization observer readout
| Local Sidereal Time | 20:00:57 |
| Azimuth | 345.576° N |
| Elevation | -21.253° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 546.084 km |
| Perigee altitude | 529.645 km |
| Semi-major axis | 6,916.002 km |
| Eccentricity | 0.0011885 |
| Inclination | 97.577° |
| RAAN | 245.3662° |
| Arg. of periapsis | 113.8702° |
| True anomaly | 246.25259° |
| Mean anomaly | 246.3773° |
| Eccentric anomaly | 246.31494° |
| Mean motion | 3.77364 °/min |
| BSTAR | 0.00058099 |
| Orbital period | 95.4 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 | 2024-12-12 05:47:04.363Z | 34.13° NE | 2024-12-12 05:50:04.363Z | 86.731° E | 27.06° | 2024-12-12 05:53:04.363Z | 154.617° SSE |
| 5 mins | 2024-12-12 18:06:04.363Z | 218.697° SW | 2024-12-12 18:08:04.363Z | 277.013° WNW | 28.048° | 2024-12-12 18:11:04.363Z | 327.608° NNW |
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