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: 15 hours ago
TLE from 15 hours ago
0 MKA-FKI 1
1 38711U 12039E 25358.26016747 .00000167 00000-0 90544-4 0 9991
2 38711 98.9583 106.5202 0010676 316.4490 43.5845 14.25343500697926Epoch: 2025-12-24T06:14Z
TLE epoch observation values (Epoch: 2025-12-24T06:14:38.469Z)
Latitude
-0.00001°
Longitude
-80.1722°
Altitude
804.698 km
Speed
7.454 km/s
True Right ascension
07h 06m 04s
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
20:54:18
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
812.17 km
Perigee altitude
796.833 km
Semi-major axis
7,182.639 km
Eccentricity
0.00107
Inclination
98.9583°
RAAN
106.5202°
Arg. of periapsis
316.449°
True anomaly
43.66892°
Mean anomaly
43.5845°
Eccentric anomaly
43.6267°
Mean motion
3.56547 °/min
Orbital period
100.97 mins
BSTAR
0.000090544
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2025-12-25 06:01:06.701Z | 83.916° E | 2025-12-25 06:03:06.701Z | 56.877° ENE | 16.411° | 2025-12-25 06:05:06.701Z | 31.666° NE |
| 9 mins | 2025-12-25 07:38:06.701Z | 180.604° SSW | 2025-12-25 07:42:06.701Z | 263.214° W | 41.475° | 2025-12-25 07:47:06.701Z | 338.974° N |
| 9 mins | 2025-12-25 19:54:06.701Z | 29.535° NE | 2025-12-25 19:58:06.701Z | 105.275° ESE | 37.795° | 2025-12-25 20:03:06.701Z | 176.213° S |
| 5 mins | 2025-12-25 21:35:06.701Z | 328.665° NNW | 2025-12-25 21:37:06.701Z | 300.93° NW | 19.467° | 2025-12-25 21:40:06.701Z | 259.76° W |
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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