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YUBELEINY 2

NORAD 38735 Payload LEO 2012-041C ● Active
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
1481 km
Apogee
1510 km
Inclination
82.5°
Period
115.9 min
Mean Motion
12.42649251 rev/day
TLE Epoch
2026-06-19 06:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude1,496 km
Orbital Velocity25,626 km/h
Velocity7.12 km/s
Orbital Period116 minutes
Orbits / Day12.43
Eccentricity0.0018
Semi-Major Axis7,867 km
Est. Orbital LifetimeThousands of years
🚀 Launch & Identity
Country / Operator
🇷🇺 Russia (CIS)
Launch Date
2012-07-28
Launch Site
PKMTR
Int'l Designator
2012-041C
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
YUBELEINY 2 is an active satellite operated by Russia (CIS), launched on 2012-07-28 from PKMTR. After 14 years in orbit, it continues to be tracked by global surveillance networks. It orbits in Low Earth Orbit (LEO) at altitudes between 1,481 km and 1,510 km with an inclination of 82.5°. It travels at approximately 25,626 km/h (7.12 km/s), completing one full orbit every 116 minutes — that’s roughly 12.43 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is thousands of years. Orbital Radar tracks YUBELEINY 2 in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
YUBELEINY 2 orbits at an average altitude of 1,496 km in the uppermost reaches of Low Earth Orbit. At this altitude, orbital decay is effectively zero without active deorbiting, and coverage footprints are significantly larger than lower LEO, though at the cost of higher latency. Within ±50 km of YUBELEINY 2’s average altitude, there are currently 247 active payloads and 249 tracked debris or rocket body fragments. With an inclination of 82.5°, YUBELEINY 2 passes over latitudes between 82.5°N and 82.5°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 1,285 active satellites in total, of which 239 share a similar altitude band with YUBELEINY 2.
❓ Frequently Asked Questions
YUBELEINY 2 orbits in Low Earth Orbit (LEO) at altitudes between 1,481 km (perigee) and 1,510 km (apogee), with an average altitude of approximately 1,496 km. It completes one orbit every 116 minutes, travelling at approximately 25,626 km/h (15,923 mph).
YUBELEINY 2 is operated by Russia (CIS). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 38735. You can track YUBELEINY 2 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
YUBELEINY 2 was launched on 2012-07-28 from PKMTR. At its current altitude, the estimated remaining orbital lifetime is: thousands of years. View the full satellite launch log.
Yes — Orbital Radar tracks YUBELEINY 2 (NORAD ID 38735) 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.
YUBELEINY 2 travels at approximately 25,626 km/h (15,923 mph) — roughly 7.12 km/s. It completes 12.43 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 25 sunrises and sunsets every 24 hours.