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TEMISAT

NORAD 22783 Payload LEO 1993-055B ● Active
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
934 km
Apogee
967 km
Inclination
82.5°
Period
104.0 min
Mean Motion
13.83896087 rev/day
TLE Epoch
2026-06-19 17:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude951 km
Orbital Velocity26,563 km/h
Velocity7.38 km/s
Orbital Period104 minutes
Orbits / Day13.84
Eccentricity0.0023
Semi-Major Axis7,322 km
Est. Orbital Lifetime~100–500 years
🚀 Launch & Identity
Country / Operator
🇮🇹 Italy
Launch Date
1993-08-31
Launch Site
PKMTR
Int'l Designator
1993-055B
Object Type
Payload
RCS Size
Medium (0.1–1 m²)
📖 About This Object
TEMISAT is an active satellite operated by Italy, launched on 1993-08-31 from PKMTR. With over 33 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Low Earth Orbit (LEO) at altitudes between 934 km and 967 km with an inclination of 82.5°. It travels at approximately 26,563 km/h (7.38 km/s), completing one full orbit every 104 minutes — that’s roughly 13.84 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~100–500 years. Orbital Radar tracks TEMISAT in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
TEMISAT orbits at an average altitude of 951 km in the upper LEO band, where atmospheric drag is negligible and objects can persist for centuries to millennia. This altitude is used by broadband constellations like OneWeb and by scientific missions requiring stable orbits far from the densest debris bands. Within ±50 km of TEMISAT’s average altitude, there are currently 324 active payloads and 1,092 tracked debris or rocket body fragments. With an inclination of 82.5°, TEMISAT 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. Italy operates approximately 88 active satellites in total.
❓ Frequently Asked Questions
TEMISAT orbits in Low Earth Orbit (LEO) at altitudes between 934 km (perigee) and 967 km (apogee), with an average altitude of approximately 951 km. It completes one orbit every 104 minutes, travelling at approximately 26,563 km/h (16,505 mph).
TEMISAT is operated by Italy. It is catalogued by the U.S. Space Surveillance Network under NORAD ID 22783. You can track TEMISAT in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
TEMISAT was launched on 1993-08-31 from PKMTR. At its current altitude, the estimated remaining orbital lifetime is: ~100–500 years. View the full satellite launch log.
Yes — Orbital Radar tracks TEMISAT (NORAD ID 22783) 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.
TEMISAT travels at approximately 26,563 km/h (16,505 mph) — roughly 7.38 km/s. It completes 13.84 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 28 sunrises and sunsets every 24 hours.