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NILESAT 102

NORAD 26470 Payload GEO 2000-046B ● Active
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
36401 km
Apogee
36445 km
Inclination
9.4°
Period
1468.7 min
Mean Motion
0.98043419 rev/day
TLE Epoch
2026-06-19 00:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude36,423 km
Orbital Velocity10,987 km/h
Velocity3.05 km/s
Orbital Period24.5 hours
Orbits / Day0.98
Eccentricity0.0005
Semi-Major Axis42,794 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
Nilesat (Egypt)
Launch Date
2000-08-17
Launch Site
Guiana Space Centre, Kourou
Int'l Designator
2000-046B
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
NILESAT 102 is an active satellite operated by Nilesat (Egypt), launched on 2000-08-17 from Guiana Space Centre, Kourou. With over 26 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Geostationary Orbit (GEO) at altitudes between 36,401 km and 36,445 km with an inclination of 9.4°. It travels at approximately 10,987 km/h (3.05 km/s), completing one full orbit every 24.5 hours — that’s roughly 0.98 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 NILESAT 102 in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
NILESAT 102 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 9.4°, 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 NILESAT 102’s average altitude, there are currently 19 active payloads and 21 tracked debris or rocket body fragments. Egypt operates approximately 12 active satellites in total.
❓ Frequently Asked Questions
NILESAT 102 orbits at approximately 36,423 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 10,987 km/h — it just keeps pace with the ground below. With an inclination of 9.4°, it actually traces a small figure-of-eight pattern rather than remaining perfectly fixed. Learn more about geostationary orbits.
NILESAT 102 is operated by Nilesat (Egypt). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 26470. You can track NILESAT 102 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
NILESAT 102 was launched on 2000-08-17 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 NILESAT 102 (NORAD ID 26470) 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.
NILESAT 102 travels at approximately 10,987 km/h (6,827 mph) — roughly 3.05 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.