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MKA PN2 (RELEK)

NORAD 40070 Payload LEO 2014-037B ● Active
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
614 km
Apogee
800 km
Inclination
98.1°
Period
98.9 min
Mean Motion
14.55655537 rev/day
TLE Epoch
2026-06-19 12:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude707 km
Orbital Velocity27,016 km/h
Velocity7.50 km/s
Orbital Period99 minutes
Orbits / Day14.56
Eccentricity0.0131
Semi-Major Axis7,078 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~25–100 years
🚀 Launch & Identity
Country / Operator
🇷🇺 Skobeltsyn Institute of Nuclear Physics (Russia (CIS))
Launch Date
2014-07-08
Launch Site
Baikonur, Kazakhstan
Int'l Designator
2014-037B
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
MKA PN2 (RELEK) is an active satellite operated by Skobeltsyn Institute of Nuclear Physics (Russia (CIS)), launched on 2014-07-08 from Baikonur, Kazakhstan. After 12 years in orbit, it continues to be tracked by global surveillance networks. It orbits in Low Earth Orbit (LEO) at altitudes between 614 km and 800 km with an inclination of 98.1°. It travels at approximately 27,016 km/h (7.50 km/s), completing one full orbit every 99 minutes — that’s roughly 14.56 orbits per day. Its near-polar, sun-synchronous orbit means it passes over any given point on Earth at approximately the same local solar time, ideal for consistent Earth observation lighting conditions. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~25–100 years. Orbital Radar tracks MKA PN2 (RELEK) in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
MKA PN2 (RELEK) orbits at an average altitude of 707 km in a sun-synchronous orbit (SSO), a specialised subset of LEO where the orbital plane precesses to maintain a constant angle relative to the Sun. This provides consistent lighting conditions on every pass — essential for Earth observation, weather monitoring and environmental science. Within ±50 km of MKA PN2 (RELEK)’s average altitude, there are currently 251 active payloads and 1,520 tracked debris or rocket body fragments — notable neighbours include TERRA, AQUA, LANDSAT 9. With an inclination of 98.1°, MKA PN2 (RELEK) passes over latitudes between 98.1°N and 98.1°S, providing near-global coverage including the polar regions. Polar and near-polar orbits are used for reconnaissance, weather monitoring and Earth-observation missions that need to image every part of the planet. Russia (CIS) operates approximately 1,286 active satellites in total, of which 9 share a similar altitude band with MKA PN2 (RELEK).
❓ Frequently Asked Questions
MKA PN2 (RELEK) is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 707 km altitude. Its 98.1° inclination causes the orbital plane to precess at exactly the rate of the Earth’s revolution around the Sun, so the satellite crosses each latitude at a consistent local solar time. It completes one orbit every 99 minutes, travelling at 27,016 km/h.
MKA PN2 (RELEK) is operated by Skobeltsyn Institute of Nuclear Physics (Russia (CIS)). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 40070. You can track MKA PN2 (RELEK) in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
MKA PN2 (RELEK) was launched on 2014-07-08 from Baikonur, Kazakhstan, the world’s first and largest operational space launch facility, located in Kazakhstan. At its current altitude, the estimated remaining orbital lifetime is: ~25–100 years. View the full satellite launch log.
Yes — Orbital Radar tracks MKA PN2 (RELEK) (NORAD ID 40070) using the latest TLE (two-line element set) data from Space-Track and CelesTrak. Open the live tracker to see its current position, altitude, speed and orbital path updated in real time. You can also browse the satellite directory to find other tracked objects.
MKA PN2 (RELEK) travels at approximately 27,016 km/h (16,787 mph) — roughly 7.50 km/s. It completes 14.56 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 29 sunrises and sunsets every 24 hours.