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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Edit Public Description
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: 10 hours ago
TLE from 10 hours ago
0 MKA PN2 (RELEK)
1 40070U 14037B 25286.22311225 .00000852 00000-0 18516-3 0 9996
2 40070 98.0433 267.7213 0132346 116.2728 245.2139 14.55204866597169Epoch: 2025-10-13T05:21Z
TLE epoch observation values (Epoch: 2025-10-13T05:21:16.898Z)
Latitude
0.00001°
Longitude
165.37191°
Altitude
752.028 km
Speed
7.457 km/s
True Right ascension
17h 50m 53s
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
09:58:09
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
799.532 km
Perigee altitude
612.026 km
Semi-major axis
7,083.916 km
Eccentricity
0.01323
Inclination
98.0433°
RAAN
267.7213°
Arg. of periapsis
116.2728°
True anomaly
243.84665°
Mean anomaly
245.2139°
Eccentric anomaly
244.52931°
Mean motion
3.64027 °/min
Orbital period
98.89 mins
BSTAR
0.00018516
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2025-10-13 21:59:50.674Z | 121.282° SE | 2025-10-13 22:02:50.674Z | 79.057° E | 23.043° | 2025-10-13 22:06:50.674Z | 14.812° NNE |
| 6 mins | 2025-10-13 23:38:50.674Z | 218.658° SW | 2025-10-13 23:40:50.674Z | 256.689° W | 26.356° | 2025-10-13 23:44:50.674Z | 322.834° NNW |
| 6 mins | 2025-10-14 11:38:50.674Z | 21.165° NNE | 2025-10-14 11:41:50.674Z | 145.268° SSE | 42.378° | 2025-10-14 11:44:50.674Z | 185.22° SSW |
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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