EGYPTSAT 2
NORAD 39678
Payload
LEO
2014-021A
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LEO · NORAD 39678
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Altitude (km)
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Longitude
🛰️ Orbital Parameters
Perigee
706 km
Apogee
706 km
Inclination
51.6°
Period
98.9 min
Mean Motion
14.56062892 rev/day
TLE Epoch
2026-06-19 05:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude706 km
Orbital Velocity27,018 km/h
Velocity7.50 km/s
Orbital Period99 minutes
Orbits / Day14.56
Eccentricity0.0000
Semi-Major Axis7,077 km
Est. Orbital Lifetime~25–100 years
🚀 Launch & Identity
Country / Operator
Egypt
Launch Date
2014-04-16
Launch Site
Baikonur, Kazakhstan
Int'l Designator
2014-021A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
EGYPTSAT 2 is an active satellite operated by Egypt, launched on 2014-04-16 from Baikonur, Kazakhstan. After 12 years in orbit, it continues to be tracked by global surveillance networks. It orbits in Low Earth Orbit (LEO) at altitudes between 706 km and 706 km with an inclination of 51.6°. It travels at approximately 27,018 km/h (7.50 km/s), completing one full orbit every 99 minutes — that’s roughly 14.56 orbits per day. 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 ~25–100 years. Orbital Radar tracks EGYPTSAT 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
EGYPTSAT 2 orbits at an average altitude of 706 km in the mid-LEO band, where atmospheric drag is minimal but radiation exposure remains manageable. Objects at this altitude persist for decades to centuries, making debris mitigation critical. This regime is popular for remote sensing constellations and scientific instruments that need stable, long-duration orbits. Within ±50 km of EGYPTSAT 2’s average altitude, there are currently 252 active payloads and 1,512 tracked debris or rocket body fragments — notable neighbours include TERRA, AQUA, LANDSAT 9. With an inclination of 51.6°, EGYPTSAT 2 passes over latitudes between 51.6°N and 51.6°S, covering most populated land masses in both hemispheres. This mid-inclination band balances global coverage with efficient launch energy requirements. Egypt operates approximately 12 active satellites in total.
❓ Frequently Asked Questions
EGYPTSAT 2 orbits in Low Earth Orbit (LEO) at altitudes between 706 km (perigee) and 706 km (apogee), with an average altitude of approximately 706 km. It completes one orbit every 99 minutes, travelling at approximately 27,018 km/h (16,788 mph).
EGYPTSAT 2 is operated by Egypt. It is catalogued by the U.S. Space Surveillance Network under NORAD ID 39678. You can track EGYPTSAT 2 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
EGYPTSAT 2 was launched on 2014-04-16 from Baikonur, Kazakhstan, the world’s first and largest operational space launch facility, located in Kazakhstan. At its current altitude, the estimated remaining orbital lifetime is: ~25–100 years. View the full satellite launch log.
Yes — Orbital Radar tracks EGYPTSAT 2 (NORAD ID 39678) 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.
EGYPTSAT 2 travels at approximately 27,018 km/h (16,788 mph) — roughly 7.50 km/s. It completes 14.56 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 29 sunrises and sunsets every 24 hours.