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: 12 hours ago
TLE from 12 hours ago
0 MKA PN2 (RELEK)
1 40070U 14037B 25346.17775710 .00001360 00000-0 29048-3 0 9997
2 40070 98.0496 325.4919 0129578 290.4354 68.2969 14.55372732605887Epoch: 2025-12-12T04:15Z
TLE epoch observation values (Epoch: 2025-12-12T04:15:58.213Z)
Latitude
-0.0001°
Longitude
-179.62376°
Altitude
678.211 km
Speed
7.535 km/s
True Right ascension
21h 41m 58s
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
14:55:15
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
797.019 km
Perigee altitude
613.449 km
Semi-major axis
7,083.371 km
Eccentricity
0.01296
Inclination
98.0496°
RAAN
325.4919°
Arg. of periapsis
290.4354°
True anomaly
69.68467°
Mean anomaly
68.2969°
Eccentric anomaly
68.98997°
Mean motion
3.64069 °/min
Orbital period
98.88 mins
BSTAR
0.00029048
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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 | 2025-12-12 22:32:14.172Z | 153.397° SSE | 2025-12-12 22:36:14.172Z | 76.784° E | 42.246° | 2025-12-12 22:41:14.172Z | 353.399° N |
| 5 mins | 2025-12-13 10:35:14.172Z | 60.109° ENE | 2025-12-13 10:37:14.172Z | 88.639° E | 19.426° | 2025-12-13 10:40:14.172Z | 131.018° SE |
| 8 mins | 2025-12-13 12:12:14.172Z | 352.512° N | 2025-12-13 12:15:14.172Z | 298.868° NW | 35.71° | 2025-12-13 12:20:14.172Z | 217.124° 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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