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IONOSFERA-M 02

NORAD 61736 Payload LEO 2024-199B ● Active
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
815 km
Apogee
817 km
Inclination
98.7°
Period
101.2 min
Mean Motion
14.22758026 rev/day
TLE Epoch
2026-06-19 21:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude816 km
Orbital Velocity26,810 km/h
Velocity7.45 km/s
Orbital Period101 minutes
Orbits / Day14.23
Eccentricity0.0001
Semi-Major Axis7,187 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~100–500 years
🚀 Launch & Identity
Country / Operator
🇷🇺 Russia (CIS)
Launch Date
2024-11-04
Launch Site
Vostochny, Russia
Int'l Designator
2024-199B
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
IONOSFERA-M 02 is an active satellite operated by Russia (CIS), launched on 2024-11-04 from Vostochny, Russia. It orbits in Low Earth Orbit (LEO) at altitudes between 815 km and 817 km with an inclination of 98.7°. It travels at approximately 26,810 km/h (7.45 km/s), completing one full orbit every 101 minutes — that’s roughly 14.23 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. Its near-circular orbit (eccentricity close to zero) means it maintains a very consistent altitude throughout each revolution. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~100–500 years. Orbital Radar tracks IONOSFERA-M 02 in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
IONOSFERA-M 02 orbits at an average altitude of 816 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 IONOSFERA-M 02’s average altitude, there are currently 407 active payloads and 2,307 tracked debris or rocket body fragments — notable neighbours include NOAA 20, ONEWEB-0179, ONEWEB-0455. With an inclination of 98.7°, IONOSFERA-M 02 passes over latitudes between 98.7°N and 98.7°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 84 share a similar altitude band with IONOSFERA-M 02.
❓ Frequently Asked Questions
IONOSFERA-M 02 is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 816 km altitude. Its 98.7° 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 101 minutes, travelling at 26,810 km/h.
IONOSFERA-M 02 is operated by Russia (CIS). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 61736. You can track IONOSFERA-M 02 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
IONOSFERA-M 02 was launched on 2024-11-04 from Vostochny, Russia. At its current altitude, the estimated remaining orbital lifetime is: ~100–500 years. View the full satellite launch log.
Yes — Orbital Radar tracks IONOSFERA-M 02 (NORAD ID 61736) 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.
IONOSFERA-M 02 travels at approximately 26,810 km/h (16,659 mph) — roughly 7.45 km/s. It completes 14.23 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 28 sunrises and sunsets every 24 hours.