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). 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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38711 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CISRelated business
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
Shape & HBR
Box + 3 Pan, 0.5 m
Radar Cross Section
1.500 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 9 hours ago
TLE from 9 hours ago
0 MKA-FKI 1
1 38711U 12039E 25260.89332466 .00000146 00000-0 81734-4 0 9999
2 38711 98.9533 7.1318 0010732 230.3943 129.6289 14.25272359684056Epoch: 2025-09-17T21:26Z
TLE epoch observation values (Epoch: 2025-09-17T21:26:23.25Z)
Latitude
-0.00001°
Longitude
48.47219°
Altitude
815.415 km
Speed
7.443 km/s
True Right ascension
00h 28m 31s
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
23:32:36
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
812.449 km
Perigee altitude
797.032 km
Semi-major axis
7,182.877 km
Eccentricity
0.00107
Inclination
98.9533°
RAAN
7.1318°
Arg. of periapsis
230.3943°
True anomaly
129.72354°
Mean anomaly
129.6289°
Eccentric anomaly
129.67623°
Mean motion
3.5653 °/min
Orbital period
100.97 mins
BSTAR
0.000081734
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Other satellites on launch #39 in the year 2012 (2012-07-22 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.MKA-FKI 1 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. |
|---|---|---|---|---|---|---|---|
| 9 mins | 2025-09-18 07:39:18.765Z | 190.283° SSW | 2025-09-18 07:44:18.765Z | 273.362° WNW | 34.539° | 2025-09-18 07:48:18.765Z | 329.962° NNW |
| 8 mins | 2025-09-18 19:56:18.765Z | 21.438° NNE | 2025-09-18 20:00:18.765Z | 138.024° SSE | 42.836° | 2025-09-18 20:04:18.765Z | 186.164° SSW |
| 4 mins | 2025-09-18 21:37:18.765Z | 321.457° NNW | 2025-09-18 21:39:18.765Z | 296.288° NW | 14.597° | 2025-09-18 21:41:18.765Z | 272.172° WNW |
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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