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KHALIFASAT

NORAD 43676 Payload LEO 2018-084F ● Active
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
560 km
Apogee
568 km
Inclination
98.1°
Period
95.9 min
Mean Motion
15.01009606 rev/day
TLE Epoch
2026-03-17 22:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude564 km
Orbital Velocity27,293 km/h
Velocity7.58 km/s
Orbital Period96 minutes
Orbits / Day15.01
Eccentricity0.0006
Semi-Major Axis6,935 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~3–10 years
🚀 Launch & Identity
Country / Operator
🇦🇪 UAE
Launch Date
2018-10-29
Launch Site
TNSTA
Int'l Designator
2018-084F
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
KHALIFASAT is an active satellite operated by UAE, launched on 2018-10-29 from TNSTA. It orbits in Low Earth Orbit (LEO) at altitudes between 560 km and 568 km with an inclination of 98.1°. It travels at approximately 27,293 km/h (7.58 km/s), completing one full orbit every 96 minutes — that’s roughly 15.01 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. Its near-circular orbit (eccentricity close to zero) means it maintains a very consistent altitude throughout each revolution. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~3–10 years. Orbital Radar tracks KHALIFASAT in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
KHALIFASAT operates in a sun-synchronous orbit (SSO), a special subset of LEO where the orbital plane precesses to keep a constant angle relative to the Sun. This means the satellite crosses any given latitude at approximately the same local solar time on every pass, providing consistent lighting conditions — essential for Earth observation, weather monitoring and environmental science. SSO orbits typically sit between 600 and 800 km altitude with inclinations near 97–99°.
❓ Frequently Asked Questions
KHALIFASAT is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 564 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 96 minutes, travelling at 27,293 km/h.
KHALIFASAT is operated by UAE. It is catalogued by the U.S. Space Surveillance Network under NORAD ID 43676. You can track KHALIFASAT in real time on Orbital Radar’s live tracker.
KHALIFASAT was launched on 2018-10-29 from TNSTA. At its current altitude, the estimated remaining orbital lifetime is: ~3–10 years.
Yes — Orbital Radar tracks KHALIFASAT (NORAD ID 43676) 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.
KHALIFASAT travels at approximately 27,293 km/h (16,959 mph) — roughly 7.58 km/s. It completes 15.01 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 30 sunrises and sunsets every 24 hours.