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ANIK F1

NORAD 26624 Payload GEO 2000-076A ● Active
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
36134 km
Apogee
36184 km
Inclination
5.2°
Period
1455.2 min
Mean Motion
0.98958097 rev/day
TLE Epoch
2026-06-19 19:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude36,159 km
Orbital Velocity11,021 km/h
Velocity3.06 km/s
Orbital Period24.3 hours
Orbits / Day0.99
Eccentricity0.0006
Semi-Major Axis42,530 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
🇨🇦 Telesat Canada Ltd. (BCE, Inc.) (Canada)
Launch Date
2000-11-21
Launch Site
Guiana Space Centre, Kourou
Int'l Designator
2000-076A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
ANIK F1 is an active satellite operated by Telesat Canada Ltd. (BCE, Inc.) (Canada), launched on 2000-11-21 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 36,134 km and 36,184 km with an inclination of 5.2°. It travels at approximately 11,021 km/h (3.06 km/s), completing one full orbit every 24.3 hours — that’s roughly 0.99 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 ANIK F1 in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
ANIK F1 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 5.2°, 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 ANIK F1’s average altitude, there are currently 166 active payloads and 9 tracked debris or rocket body fragments. Canada operates approximately 67 active satellites in total, of which 3 share a similar altitude band with ANIK F1.
❓ Frequently Asked Questions
ANIK F1 orbits at approximately 36,159 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 11,021 km/h — it just keeps pace with the ground below. With an inclination of 5.2°, it actually traces a small figure-of-eight pattern rather than remaining perfectly fixed. Learn more about geostationary orbits.
ANIK F1 is operated by Telesat Canada Ltd. (BCE, Inc.) (Canada). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 26624. You can track ANIK F1 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
ANIK F1 was launched on 2000-11-21 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 ANIK F1 (NORAD ID 26624) 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.
ANIK F1 travels at approximately 11,021 km/h (6,848 mph) — roughly 3.06 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.