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INSAT 2E (APR-1)

NORAD 25666 Payload GEO 1999-016A ● Active
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
35920 km
Apogee
35998 km
Inclination
11.3°
Period
1444.9 min
Mean Motion
0.99659800 rev/day
TLE Epoch
2026-06-18 19:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude35,959 km
Orbital Velocity11,047 km/h
Velocity3.07 km/s
Orbital Period~24 hours (geosynchronous)
Orbits / Day1.00
Eccentricity0.0009
Semi-Major Axis42,330 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
🇮🇳 India
Launch Date
1999-04-02
Launch Site
Guiana Space Centre, Kourou
Int'l Designator
1999-016A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
INSAT 2E (APR-1) is an active satellite operated by India, launched on 1999-04-02 from Guiana Space Centre, Kourou. With over 27 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Geostationary Orbit (GEO) at altitudes between 35,920 km and 35,998 km with an inclination of 11.3°. It travels at approximately 11,047 km/h (3.07 km/s), completing one full orbit every ~24 hours (geosynchronous) — that’s roughly 1.00 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 INSAT 2E (APR-1) in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
INSAT 2E (APR-1) 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 11.3°, 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 INSAT 2E (APR-1)’s average altitude, there are currently 57 active payloads and 19 tracked debris or rocket body fragments. India operates approximately 108 active satellites in total, of which 4 share a similar altitude band with INSAT 2E (APR-1).
❓ Frequently Asked Questions
INSAT 2E (APR-1) orbits at approximately 35,959 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 11,047 km/h — it just keeps pace with the ground below. With an inclination of 11.3°, it actually traces a small figure-of-eight pattern rather than remaining perfectly fixed. Learn more about geostationary orbits.
INSAT 2E (APR-1) is operated by India. It is catalogued by the U.S. Space Surveillance Network under NORAD ID 25666. You can track INSAT 2E (APR-1) in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
INSAT 2E (APR-1) was launched on 1999-04-02 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 INSAT 2E (APR-1) (NORAD ID 25666) 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.
INSAT 2E (APR-1) travels at approximately 11,047 km/h (6,864 mph) — roughly 3.07 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.