Skip to content
Home Library Satellite Directory IMECE

IMECE

NORAD 56178 Payload LEO 2023-054A ● Active
CONNECTING… LEO · NORAD 56178
NOW PASSING OVER
Calculating position…
Altitude (km)
Speed (km/s)
Latitude
Longitude
Real-time tracking powered by Orbital Radar
ORBITAL RADAR · LIVE GROUND TRACK
🌍 Track on 3D Globe
🛰️ Orbital Parameters
Perigee
667 km
Apogee
681 km
Inclination
98.1°
Period
98.2 min
Mean Motion
14.65849068 rev/day
TLE Epoch
2026-06-19 06:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude674 km
Orbital Velocity27,079 km/h
Velocity7.52 km/s
Orbital Period98 minutes
Orbits / Day14.66
Eccentricity0.0010
Semi-Major Axis7,045 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~10–25 years
🚀 Launch & Identity
Country / Operator
TÜBİTAK Space Technologies Research Institute (Turkey)
Launch Date
2023-04-15
Launch Site
Vandenberg SFB, California
Int'l Designator
2023-054A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
IMECE is an active satellite operated by TÜBİTAK Space Technologies Research Institute (Turkey), launched on 2023-04-15 from Vandenberg SFB, California. It orbits in Low Earth Orbit (LEO) at altitudes between 667 km and 681 km with an inclination of 98.1°. It travels at approximately 27,079 km/h (7.52 km/s), completing one full orbit every 98 minutes — that’s roughly 14.66 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 ~10–25 years. Orbital Radar tracks IMECE in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
IMECE orbits at an average altitude of 674 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 IMECE’s average altitude, there are currently 557 active payloads and 1,233 tracked debris or rocket body fragments — notable neighbours include TERRA, AQUA, LANDSAT 9. With an inclination of 98.1°, IMECE passes over latitudes between 98.1°N and 98.1°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. Turkey operates approximately 41 active satellites in total, of which 6 share a similar altitude band with IMECE.
❓ Frequently Asked Questions
IMECE is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 674 km altitude. Its 98.1° 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 98 minutes, travelling at 27,079 km/h.
IMECE is operated by TÜBİTAK Space Technologies Research Institute (Turkey). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 56178. You can track IMECE in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
IMECE was launched on 2023-04-15 from Vandenberg SFB, California, primarily used for polar and sun-synchronous orbit launches due to its southward ocean trajectory from California. At its current altitude, the estimated remaining orbital lifetime is: ~10–25 years. View the full satellite launch log.
Yes — Orbital Radar tracks IMECE (NORAD ID 56178) 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.
IMECE travels at approximately 27,079 km/h (16,826 mph) — roughly 7.52 km/s. It completes 14.66 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 29 sunrises and sunsets every 24 hours.