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INSAT 2E (APR-1)

NORAD 25666 Payload GEO 1999-016A ● Active
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🛰️ Orbital Parameters
Perigee
35921 km
Apogee
36002 km
Inclination
11.6°
Period
1445.1 min
Mean Motion
0.99649795 rev/day
TLE Epoch
2026-11-02 20:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude35,962 km
Orbital Velocity11,047 km/h
Velocity3.07 km/s
Orbital Period~24 hours (geosynchronous)
Orbits / Day1.00
Eccentricity0.0010
Semi-Major Axis42,333 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
🇮🇳 ISRO (India)
Launch Date
1999-04-02
Launch Site
Guiana Space Centre, French Guiana
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 ISRO (India), launched on 1999-04-02 from Guiana Space Centre, French Guiana on the Insat 2E launch. With over 27 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Geostationary Orbit (GEO) at altitudes between 35,921 km and 36,002 km with an inclination of 11.6°. 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 11.6°, 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 67 active payloads and 21 tracked debris or rocket body fragments. India operates approximately 111 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 35,962 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 11.6°, 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 ISRO (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, French Guiana. 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) orbital data in its live tracking catalogue (see our data sources). 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.