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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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, 0.9 m
Radar Cross Section
1.500 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 5 hours ago
TLE from 5 hours ago
0 MKA-FKI 1
1 38711U 12039E 26265.26472586 .00000078 00000-0 52840-4 0 9994
2 38711 98.9821 24.5512 0010521 246.2544 113.7532 14.25454591736675Epoch: 2026-09-22T06:21Z
TLE epoch observation values (Epoch: 2026-09-22T06:21:12.314Z)
Latitude
0.00004°
Longitude
-71.88281°
Altitude
812.93 km
Speed
7.445 km/s
True Right ascension
01h 38m 12s
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
04:29:16
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
811.686 km
Perigee altitude
796.573 km
Semi-major axis
7,182.266 km
Eccentricity
0.00105
Inclination
98.9821°
RAAN
24.5512°
Arg. of periapsis
246.2544°
True anomaly
113.86349°
Mean anomaly
113.7532°
Eccentric anomaly
113.80835°
Mean motion
3.56575 °/min
Orbital period
100.96 mins
BSTAR
0.00005284
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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. |
|---|---|---|---|---|---|---|---|
| 10 mins | 2026-09-22 20:24:23.270Z | 27.88° NE | 2026-09-22 20:29:23.270Z | 97.767° ESE | 42.58° | 2026-09-22 20:34:23.270Z | 170.059° S |
| 6 mins | 2026-09-22 22:06:23.270Z | 333.326° NNW | 2026-09-22 22:09:23.270Z | 287.333° WNW | 23.905° | 2026-09-22 22:12:23.270Z | 248.463° W |
| 8 mins | 2026-09-23 07:45:23.270Z | 150.001° SSE | 2026-09-23 07:49:23.270Z | 42.354° NE | 62.884° | 2026-09-23 07:53:23.270Z | 353.409° N |
| 4 mins | 2026-09-23 09:27:23.270Z | 247.182° WSW | 2026-09-23 09:29:23.270Z | 271.982° WNW | 14.748° | 2026-09-23 09:31:23.270Z | 295.753° NW |
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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