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: 4 days ago
TLE from 4 days ago
0 MKA PN2 (RELEK)
1 40070U 14037B 26154.48415706 .00000692 00000-0 15108-3 0 9994
2 40070 98.0689 132.8504 0131561 111.1700 250.3614 14.55634149631096Epoch: 2026-06-03T11:37Z
TLE epoch observation values (Epoch: 2026-06-03T11:37:11.169Z)
Latitude
-0.0001°
Longitude
66.61176°
Altitude
742.707 km
Speed
7.466 km/s
True Right ascension
08h 51m 24s
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
04:18:04
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
797.565 km
Perigee altitude
611.208 km
Semi-major axis
7,082.523 km
Eccentricity
0.01316
Inclination
98.0689°
RAAN
132.8504°
Arg. of periapsis
111.17°
True anomaly
248.94946°
Mean anomaly
250.3614°
Eccentric anomaly
249.65464°
Mean motion
3.64134 °/min
Orbital period
98.86 mins
BSTAR
0.00015108
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-06-07 21:21:55.445Z | 100.548° ESE | 2026-06-07 21:23:55.445Z | 73.374° E | 15.241° | 2026-06-07 21:26:55.445Z | 29.531° NE |
| 7 mins | 2026-06-07 22:58:55.445Z | 193.069° SSW | 2026-06-07 23:01:55.445Z | 259.657° W | 36.172° | 2026-06-07 23:05:55.445Z | 333.653° NNW |
| 6 mins | 2026-06-08 10:59:55.445Z | 43.176° NE | 2026-06-08 11:01:55.445Z | 94.614° ESE | 33.859° | 2026-06-08 11:05:55.445Z | 169.144° S |
| 4 mins | 2026-06-08 12:37:55.445Z | 320.993° NNW | 2026-06-08 12:39:55.445Z | 288.664° WNW | 16.111° | 2026-06-08 12:41:55.445Z | 259.508° 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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