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MTG-I2

NORAD 100530 Payload MEO 2026-198A ● Active
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
249 km
Apogee
35650 km
Inclination
6.0°
Period
629.4 min
Mean Motion
2.28800618 rev/day
TLE Epoch
2026-08-29 09:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude17,950 km
Orbital Velocity14,574 km/h
Velocity4.05 km/s
Orbital Period10 hours 29 minutes
Orbits / Day2.29
Eccentricity0.7278
Semi-Major Axis24,321 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
ESA (European Space Agency)
Launch Date
2026-08-27
Launch Site
Guiana Space Centre, Kourou
Int'l Designator
2026-198A
Object Type
Payload
RCS Size
Unknown
📖 About This Object
MTG-I2 is an active satellite operated by ESA (European Space Agency), launched on 2026-08-27 from Guiana Space Centre, Kourou on the MTG-I2 launch. As a relatively recent addition to the catalogue, its orbital elements are well-characterised. It orbits in Medium Earth Orbit (MEO) at altitudes between 249 km and 35,650 km with an inclination of 6.0°. It travels at approximately 14,574 km/h (4.05 km/s), completing one full orbit every 10 hours 29 minutes — that’s roughly 2.29 orbits per day. Its orbital eccentricity of 0.7278 gives it a noticeably elliptical path, with significant altitude variation between perigee and apogee. Orbital Radar tracks MTG-I2 in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
MTG-I2 orbits at an average altitude of 17,950 km in Medium Earth Orbit, the region between LEO and GEO (2,000–35,786 km). MEO’s higher altitude gives each satellite a much larger ground footprint than LEO, meaning fewer spacecraft are needed for global coverage — but signal latency is higher and radiation from the Van Allen belts is a significant design constraint. Within ±50 km of MTG-I2’s average altitude, there are currently 1 active payload and 13 tracked debris or rocket body fragments. This is a relatively sparse altitude band, containing less than 1% of all active satellites. With an inclination of 6.0°, MTG-I2 passes over latitudes between 6.0°N and 6.0°S, concentrating coverage over equatorial and near-equatorial regions. Low-inclination orbits maximise revisit rates over specific tropical zones. ESA (European Space Agency) operates approximately 82 active satellites in total.
❓ Frequently Asked Questions
MTG-I2 orbits in Medium Earth Orbit (MEO) at altitudes between 249 km (perigee) and 35,650 km (apogee), with an average altitude of approximately 17,950 km. It completes one orbit every 10 hours 29 minutes, travelling at approximately 14,574 km/h (9,056 mph).
MTG-I2 is operated by ESA (European Space Agency). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 100530. You can track MTG-I2 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
MTG-I2 was launched on 2026-08-27 from Guiana Space Centre, Kourou, the European spaceport in French Guiana, chosen for its equatorial location which provides an energy-efficient boost for orbital insertions. At its current altitude, the estimated remaining orbital lifetime is: effectively permanent — above atmospheric drag. View the full satellite launch log.
Yes — Orbital Radar tracks MTG-I2 (NORAD ID 100530) 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.
MTG-I2 travels at approximately 14,574 km/h (9,056 mph) — roughly 4.05 km/s. It completes 2.29 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 5 sunrises and sunsets every 24 hours.