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: 21 hours ago
TLE from 21 hours ago
0 MKA PN2 (RELEK)
1 40070U 14037B 25347.96528983 .00001105 00000-0 23811-3 0 9992
2 40070 98.0497 327.2153 0129518 284.8269 73.8612 14.55376657606141Epoch: 2025-12-13T23:10Z
TLE epoch observation values (Epoch: 2025-12-13T23:10:01.041Z)
Latitude
-0.00001°
Longitude
-103.17403°
Altitude
686.712 km
Speed
7.526 km/s
True Right ascension
21h 48m 51s
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
18:55:03
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
796.964 km
Perigee altitude
613.479 km
Semi-major axis
7,083.359 km
Eccentricity
0.01295
Inclination
98.0497°
RAAN
327.2153°
Arg. of periapsis
284.8269°
True anomaly
75.29317°
Mean anomaly
73.8612°
Eccentric anomaly
74.57656°
Mean motion
3.6407 °/min
Orbital period
98.88 mins
BSTAR
0.00023811
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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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2025-12-14 22:23:30.926Z | 145.936° SSE | 2025-12-14 22:27:30.926Z | 71.243° E | 38.86° | 2025-12-14 22:31:30.926Z | 359.645° N |
| 4 mins | 2025-12-15 00:04:30.926Z | 252.377° W | 2025-12-15 00:05:30.926Z | 266.69° W | 15.954° | 2025-12-15 00:08:30.926Z | 305.229° NW |
| 5 mins | 2025-12-15 10:26:30.926Z | 63.602° ENE | 2025-12-15 10:28:30.926Z | 90.091° ESE | 16.245° | 2025-12-15 10:31:30.926Z | 128.032° SE |
| 8 mins | 2025-12-15 12:03:30.926Z | 357.368° N | 2025-12-15 12:06:30.926Z | 299.417° NW | 39.43° | 2025-12-15 12:11:30.926Z | 210.783° 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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