ITAMSAT
NORAD 22826
Payload
LEO
1993-061D
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LEO · NORAD 22826
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Altitude (km)
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Speed (km/s)
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Latitude
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Longitude
🛰️ Orbital Parameters
Perigee
780 km
Apogee
794 km
Inclination
98.7°
Period
100.6 min
Mean Motion
14.31369842 rev/day
TLE Epoch
2026-06-19 16:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude787 km
Orbital Velocity26,864 km/h
Velocity7.46 km/s
Orbital Period101 minutes
Orbits / Day14.31
Eccentricity0.0010
Semi-Major Axis7,158 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~25–100 years
🚀 Launch & Identity
Country / Operator
🇮🇹 Italy
Launch Date
1993-09-26
Launch Site
Guiana Space Centre, Kourou
Int'l Designator
1993-061D
Object Type
Payload
RCS Size
Medium (0.1–1 m²)
📖 About This Object
ITAMSAT is an active satellite operated by Italy, launched on 1993-09-26 from Guiana Space Centre, Kourou. With over 33 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Low Earth Orbit (LEO) at altitudes between 780 km and 794 km with an inclination of 98.7°. It travels at approximately 26,864 km/h (7.46 km/s), completing one full orbit every 101 minutes — that’s roughly 14.31 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 ITAMSAT in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
ITAMSAT orbits at an average altitude of 787 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 ITAMSAT’s average altitude, there are currently 418 active payloads and 2,224 tracked debris or rocket body fragments — notable neighbours include NOAA 20, ONEWEB-0179, ONEWEB-0455. With an inclination of 98.7°, ITAMSAT 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. Italy operates approximately 88 active satellites in total.
❓ Frequently Asked Questions
ITAMSAT is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 787 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 26,864 km/h.
ITAMSAT is operated by Italy. It is catalogued by the U.S. Space Surveillance Network under NORAD ID 22826. You can track ITAMSAT in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
ITAMSAT was launched on 1993-09-26 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: ~25–100 years. View the full satellite launch log.
Yes — Orbital Radar tracks ITAMSAT (NORAD ID 22826) 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.
ITAMSAT travels at approximately 26,864 km/h (16,693 mph) — roughly 7.46 km/s. It completes 14.31 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 29 sunrises and sunsets every 24 hours.