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: 22 hours ago
TLE from 22 hours ago
0 MKA PN2 (RELEK)
1 40070U 14037B 25255.69279625 .00000322 00000-0 76962-4 0 9992
2 40070 98.0385 238.3239 0130445 210.9741 148.3718 14.55151190592726Epoch: 2025-09-12T16:37Z
TLE epoch observation values (Epoch: 2025-09-12T16:37:37.595Z)
Latitude
-0.00008°
Longitude
-3.01959°
Altitude
790.915 km
Speed
7.417 km/s
True Right ascension
15h 53m 17s
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
07:30:15
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
798.362 km
Perigee altitude
613.545 km
Semi-major axis
7,084.09 km
Eccentricity
0.01304
Inclination
98.0385°
RAAN
238.3239°
Arg. of periapsis
210.9741°
True anomaly
149.14491°
Mean anomaly
148.3718°
Eccentric anomaly
148.75942°
Mean motion
3.64013 °/min
Orbital period
98.9 mins
BSTAR
0.000076962
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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. |
|---|---|---|---|---|---|---|---|
| 9 mins | 2025-09-13 22:27:18.716Z | 144.2° SSE | 2025-09-13 22:31:18.716Z | 88.366° E | 37.169° | 2025-09-13 22:36:18.716Z | 359.566° N |
| 6 mins | 2025-09-14 00:07:18.716Z | 233.608° WSW | 2025-09-14 00:09:18.716Z | 260.043° W | 18.361° | 2025-09-14 00:13:18.716Z | 311.424° NW |
| 7 mins | 2025-09-14 12:07:18.716Z | 1.357° NNE | 2025-09-14 12:10:18.716Z | 314.389° NW | 39.188° | 2025-09-14 12:14:18.716Z | 210.864° SW |
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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