MKA-FKI 1, 38711
Orbit data source: Space-Track
MKA-FKI 1, 38711 is a Commonwealth of Independent States-origin payload satellite in SSO that was launched on Sun, 22 Jul 2012 UTC via a SOYUZ-FG launch vehicle from the Tyuratam Missile And Space Complex (TTMTR). 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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38711 intel report (Beta)
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MKA-FKI 1 details
| Identifier | |
| Orbit | SSO |
| Last TLE update | 18 hours ago |
| Origin | |
| Manufacturer | Lavochkin |
| Mission | Operational Civil Science |
| Bus & Motor | KARAT, Unknown motor |
| Mass | 110 kg wet, 110 kg dry |
| Launch date (UTC) | |
| Launch vehicle | |
| Launch site | |
| Object type | Payload Rocket body Debris |
| Shape & HBR | Box + 3 Pan, 1 m |
| Radar Cross Section | 1.500 m², Large (>1 m²) |
Expand to show TLE details & history
TLE from 18 hours ago
0 MKA-FKI 1
1 38711U 12039E 24296.21988730 .00000458 00000-0 21545-3 0 9993
2 38711 98.9468 30.0416 0012469 107.1007 253.1538 14.24986284636952Epoch: 2024-10-22T05:16Z
Definitive object data (Epoch: 2024-10-22T05:16:38.262Z)
| Latitude | -0.00005° |
| Longitude | -80.25315° |
| Altitude | 814.06 km |
| Speed | 7.445 km/s |
| True Right ascension | 02h 00m 09s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in full shadow at TLE epoch |
Visualization TLE readout
| Latitude | -34.39713° |
| Longitude | -73.31831° |
| Altitude | 828.293 km |
| Speed | 7.434 km/s |
| Apparent Right ascension | 04h 23m 00s |
| Apparent Declination | -41° 28' 01" |
| Sunlit | Object is in full shadow |
Visualization observer readout
| Local Sidereal Time | 18:46:10 |
| Azimuth | 105.054° ESE |
| Elevation | -63.011° |
| Doppler factor | 1 |
Orbital elements
| Apogee | 814.66 km |
| Perigee | 796.745 km |
| Semi-major axis | 7,183.839 km |
| Eccentricity | 0.0012469 |
| Inclination | 98.9468° |
| RAAN | 30.0416° |
| Arg. of periapsis | 107.1007° |
| True anomaly | 253.01711° |
| Mean anomaly | 253.1538° |
| Eccentric anomaly | 253.08545° |
| Mean motion | 3.56458 °/min |
| BSTAR | 0.00021545 |
| Period | 100.99 mins |
No data available
No data available
Other satellites on launch #39 in the year 2012 (2012-07-22 UTC)
| KANOPUS-V 1, 38707 |
| BKA 2, 38708 (Decayed) |
| EXACTVIEW-1, 38709 |
| TET-1, 38710 (Decayed) |
| MKA-FKI 1, 38711 |
| FREGAT R/B, 38712 (Decayed) |
| SL-26 R/B, 38713 (Decayed) |
| TET-1 DEB, 44597 (Decayed) |
MKA-FKI 1 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 | 2024-10-23 05:02:05.030Z | 98.892° ESE | 2024-10-23 05:05:05.030Z | 62.22° ENE | 16.599° | 2024-10-23 05:08:05.030Z | 25.283° NE |
| 8 mins | 2024-10-23 06:41:05.030Z | 183.673° SSW | 2024-10-23 06:44:05.030Z | 239.547° WSW | 40.857° | 2024-10-23 06:49:05.030Z | 337.713° N |
| 8 mins | 2024-10-23 18:57:05.030Z | 31.811° NE | 2024-10-23 19:00:05.030Z | 85.317° E | 37.623° | 2024-10-23 19:05:05.030Z | 175.202° S |
| 5 mins | 2024-10-23 20:38:05.030Z | 322.737° NNW | 2024-10-23 20:40:05.030Z | 293.418° NW | 18.885° | 2024-10-23 20:43:05.030Z | 255.433° W |