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). Payloads include a variety of satellites, spacecraft, and rockets 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)
MKA PN2 (RELEK) details
| Identifier | |
| Orbit | SSO |
| Last TLE update | 22 hours ago |
| Origin | |
| 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 | Payload Rocket body Debris |
| Shape & HBR | Box, 1 m |
| Radar Cross Section | 1.500 m², Large (>1 m²) |
Expand to show TLE details & history
TLE from 22 hours ago
0 MKA PN2 (RELEK)
1 40070U 14037B 24360.55888263 .00002413 00000-0 51485-3 0 9992
2 40070 98.0140 347.4363 0131427 303.6359 55.2356 14.54527558554750Epoch: 2024-12-25T13:24Z
Definitive object data (Epoch: 2024-12-25T13:24:47.459Z)
| Latitude | 0° |
| Longitude | 51.68766° |
| Altitude | 661.583 km |
| Speed | 7.554 km/s |
| True Right ascension | 23h 09m 44s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
| Latitude | 48.62035° |
| Longitude | 43.40746° |
| Altitude | 746.737 km |
| Speed | 7.471 km/s |
| Apparent Right ascension | 22h 31m 52s |
| Apparent Declination | 7° 25' 14" |
| Sunlit | Object is in daylight |
Visualization observer readout
| Local Sidereal Time | 10:27:18 |
| Azimuth | 358.459° N |
| Elevation | -42.652° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 801.109 km |
| Perigee altitude | 614.848 km |
| Semi-major axis | 7,086.116 km |
| Eccentricity | 0.0131427 |
| Inclination | 98.014° |
| RAAN | 347.4363° |
| Arg. of periapsis | 303.6359° |
| True anomaly | 56.48442° |
| Mean anomaly | 55.2356° |
| Eccentric anomaly | 55.85884° |
| Mean motion | 3.63857 °/min |
| BSTAR | 0.00051485 |
| Orbital period | 98.94 mins |
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Other satellites on launch #37 in the year 2014 (2014-07-08 UTC)
| METEOR M2, 40069 |
| MKA PN2 (RELEK), 40070 |
| DX 1, 40071 |
| SKYSAT 2, 40072 |
| DUMMY SAT, 40073 |
| UKUBE 1, 40074 |
| AISSAT 2, 40075 |
| TDS 1, 40076 |
| SL-4 R/B, 40077 (Decayed) |
| FREGAT DEB, 40078 |
MKA PN2 (RELEK) Visibility forecast
Observer location: undefined°, undefined
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 | 2024-12-26 11:28:00.801Z | 38.037° NE | 2024-12-26 11:32:00.801Z | 99.497° ESE | 28.174° | 2024-12-26 11:36:00.801Z | 156.174° SSE |
| 7 mins | 2024-12-26 13:07:00.801Z | 337.092° NNW | 2024-12-26 13:10:00.801Z | 284.096° WNW | 26.996° | 2024-12-26 13:14:00.801Z | 232.588° WSW |
| 7 mins | 2024-12-26 22:35:00.801Z | 117.85° SE | 2024-12-26 22:38:00.801Z | 62.49° ENE | 27.127° | 2024-12-26 22:42:00.801Z | 8.224° NNE |
| 6 mins | 2024-12-27 00:13:00.801Z | 219.303° SW | 2024-12-27 00:16:00.801Z | 273.056° WNW | 24.693° | 2024-12-27 00:19:00.801Z | 317.452° NNW |
Authenticating...
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