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, 0.9 m
Radar Cross Section
1.500 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 23 hours ago
TLE from 23 hours ago
0 MKA PN2 (RELEK)
1 40070U 14037B 26296.35479578 .00000595 00000-0 13140-3 0 9990
2 40070 98.0878 270.1865 0130742 30.9259 329.9555 14.55767485651739Epoch: 2026-10-23T08:30Z
TLE epoch observation values (Epoch: 2026-10-23T08:30:54.355Z)
Latitude
-0.00008°
Longitude
110.6835°
Altitude
629.964 km
Speed
7.586 km/s
True Right ascension
18h 00m 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
02:41:21
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
796.547 km
Perigee altitude
611.362 km
Semi-major axis
7,082.091 km
Eccentricity
0.01307
Inclination
98.0878°
RAAN
270.1865°
Arg. of periapsis
30.9259°
True anomaly
329.19466°
Mean anomaly
329.9555°
Eccentric anomaly
329.57616°
Mean motion
3.64167 °/min
Orbital period
98.86 mins
BSTAR
0.0001314
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-10-24 09:51:57.177Z | 66.726° ENE | 2026-10-24 09:53:57.177Z | 90.908° ESE | 12.328° | 2026-10-24 09:55:57.177Z | 114.704° SE |
| 8 mins | 2026-10-24 11:28:57.177Z | 4.829° NNE | 2026-10-24 11:31:57.177Z | 304.369° NW | 69.86° | 2026-10-24 11:36:57.177Z | 202.48° SSW |
| 7 mins | 2026-10-24 22:34:57.177Z | 178.291° S | 2026-10-24 22:37:57.177Z | 257.838° W | 67.392° | 2026-10-24 22:41:57.177Z | 341.236° N |
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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