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ITALSAT 2

NORAD 24208 Payload GEO 1996-044A ● Active
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
35542 km
Apogee
35744 km
Inclination
13.8°
Period
1428.8 min
Mean Motion
1.00786485 rev/day
TLE Epoch
2026-06-19 10:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude35,643 km
Orbital Velocity11,089 km/h
Velocity3.08 km/s
Orbital Period23 hours 49 minutes
Orbits / Day1.01
Eccentricity0.0024
Semi-Major Axis42,014 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
🇮🇹 Italy
Launch Date
1996-08-08
Launch Site
Guiana Space Centre, Kourou
Int'l Designator
1996-044A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
ITALSAT 2 is an active satellite operated by Italy, launched on 1996-08-08 from Guiana Space Centre, Kourou. With over 30 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Geostationary Orbit (GEO) at altitudes between 35,542 km and 35,744 km with an inclination of 13.8°. It travels at approximately 11,089 km/h (3.08 km/s), completing one full orbit every 23 hours 49 minutes — that’s roughly 1.01 orbits per day. At geostationary altitude, there is no meaningful atmospheric drag — this object will remain in orbit indefinitely unless actively deorbited. Orbital Radar tracks ITALSAT 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
ITALSAT 2 occupies geostationary orbit at approximately 35,786 km above the equator, where its orbital period matches the Earth’s 24-hour rotation. From the ground, it appears to hover over a fixed point — ideal for broadcast television, weather monitoring and wideband communications. With an inclination of 13.8°, it traces a small figure-of-eight pattern relative to the equator rather than remaining perfectly stationary, which can indicate aging stationkeeping fuel or a deliberate inclined-orbit strategy. Within ±50 km of ITALSAT 2’s average altitude, there are currently 9 active payloads and 25 tracked debris or rocket body fragments. Italy operates approximately 88 active satellites in total.
❓ Frequently Asked Questions
ITALSAT 2 orbits at approximately 35,643 km altitude, where the orbital period matches the Earth’s 24-hour rotation. This means it stays above the same point on the equator at all times. Its actual speed is still 11,089 km/h — it just keeps pace with the ground below. With an inclination of 13.8°, it actually traces a small figure-of-eight pattern rather than remaining perfectly fixed. Learn more about geostationary orbits.
ITALSAT 2 is operated by Italy. It is catalogued by the U.S. Space Surveillance Network under NORAD ID 24208. You can track ITALSAT 2 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
ITALSAT 2 was launched on 1996-08-08 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. View the full satellite launch log.
Yes — Orbital Radar tracks ITALSAT 2 (NORAD ID 24208) 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.
ITALSAT 2 travels at approximately 11,089 km/h (6,890 mph) — roughly 3.08 km/s. Despite this high speed, it appears stationary from the ground because it matches the Earth’s rotation. Geostationary satellites are actually slower than LEO satellites because orbital velocity decreases with altitude.