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ANIK E2

NORAD 21222 Payload GEO 1991-026A ● Active
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
36082 km
Apogee
36138 km
Inclination
14.1°
Period
1452.7 min
Mean Motion
0.99128475 rev/day
TLE Epoch
2026-05-08 12:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude36,110 km
Orbital Velocity11,027 km/h
Velocity3.06 km/s
Orbital Period24.2 hours
Orbits / Day0.99
Eccentricity0.0007
Semi-Major Axis42,481 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
🇨🇦 Canada
Launch Date
1991-04-04
Launch Site
Guiana Space Centre, Kourou
Int'l Designator
1991-026A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
ANIK E2 is an active satellite operated by Canada, launched on 1991-04-04 from Guiana Space Centre, Kourou. With over 35 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Geostationary Orbit (GEO) at altitudes between 36,082 km and 36,138 km with an inclination of 14.1°. It travels at approximately 11,027 km/h (3.06 km/s), completing one full orbit every 24.2 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 E2 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 E2 occupies geostationary orbit (GEO) at approximately 35,786 km above the equator. At this precise altitude, the satellite’s orbital period matches the Earth’s rotation — so it appears to hover over a fixed point on the equator. GEO is used primarily for broadcast television, weather monitoring (Meteosat, GOES) and wideband communications. Only about 560 active satellites occupy the GEO belt, but its commercial value is immense: a single GEO slot can cover roughly one-third of the Earth’s surface. This satellite has a non-zero inclination of 14.1°, meaning it traces a small figure-of-eight pattern relative to the ground rather than remaining perfectly stationary. This can indicate an aging satellite whose stationkeeping fuel is running low, or a deliberate inclined-orbit strategy to extend operational life.
❓ Frequently Asked Questions
ANIK E2 orbits at approximately 36,110 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 11,027 km/h — it just keeps pace with the ground below. With an inclination of 14.1°, it actually traces a small figure-of-eight pattern rather than remaining perfectly fixed.
ANIK E2 is operated by Canada. It is catalogued by the U.S. Space Surveillance Network under NORAD ID 21222. You can track ANIK E2 in real time on Orbital Radar’s live tracker.
ANIK E2 was launched on 1991-04-04 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.
Yes — Orbital Radar tracks ANIK E2 (NORAD ID 21222) 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.
ANIK E2 travels at approximately 11,027 km/h (6,852 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.
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