MKA PN2 (RELEK), 40070
Orbit data source: Space-Track
MKA PN2 (RELEK), 40070 is a Commonwealth of Independent States-origin payload satellite in SSO that was launched on Tue, 08 Jul 2014 UTC via a SOYUZ-2-1B 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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40070 intel report (Beta)
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Identifier
Orbit
Country
CISRelated business
Manufacturer
Lavochkin
Mission
Non-operational Civil Science
Bus & Motor
KARAT, Unknown motor
Mass
288 kg wet, 288 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 0.5 m
Radar Cross Section
1.500 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 11 hours ago
TLE from 11 hours ago
0 MKA PN2 (RELEK)
1 40070U 14037B 26251.19638110 .00000249 00000-0 60989-4 0 9992
2 40070 98.0800 226.4347 0130204 170.1744 190.2047 14.55729785645168Epoch: 2026-09-08T04:42Z
TLE epoch observation values (Epoch: 2026-09-08T04:42:47.327Z)
Latitude
-0°
Longitude
168.47124°
Altitude
800.827 km
Speed
7.405 km/s
True Right ascension
15h 05m 44s
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
07:41:19
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
796.29 km
Perigee altitude
611.863 km
Semi-major axis
7,082.214 km
Eccentricity
0.01302
Inclination
98.08°
RAAN
226.4347°
Arg. of periapsis
170.1744°
True anomaly
189.94454°
Mean anomaly
190.2047°
Eccentric anomaly
190.0742°
Mean motion
3.64158 °/min
Orbital period
98.86 mins
BSTAR
0.000060989
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Other satellites on launch #37 in the year 2014 (2014-07-08 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 PN2 (RELEK) 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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-09-08 21:21:57.447Z | 108.678° ESE | 2026-09-08 21:24:57.447Z | 66.524° ENE | 22.286° | 2026-09-08 21:27:57.447Z | 23.636° NE |
| 8 mins | 2026-09-08 22:58:57.447Z | 196.446° SSW | 2026-09-08 23:02:57.447Z | 275.917° WNW | 42.265° | 2026-09-08 23:06:57.447Z | 331.752° NNW |
| 7 mins | 2026-09-09 10:59:57.447Z | 28.082° NE | 2026-09-09 11:02:57.447Z | 92.394° ESE | 51.104° | 2026-09-09 11:06:57.447Z | 175.524° S |
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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