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INSAT 4CR

NORAD 32050 Payload GEO 2007-037A ● Active
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
36084 km
Apogee
36087 km
Inclination
6.9°
Period
1451.4 min
Mean Motion
0.99215971 rev/day
TLE Epoch
2026-06-19 05:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude36,086 km
Orbital Velocity11,031 km/h
Velocity3.06 km/s
Orbital Period24.2 hours
Orbits / Day0.99
Eccentricity0.0000
Semi-Major Axis42,457 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
🇮🇳 India
Launch Date
2007-09-02
Launch Site
SRI
Int'l Designator
2007-037A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
INSAT 4CR is an active satellite operated by India, launched on 2007-09-02 from SRI. After 19 years in orbit, it continues to be tracked by global surveillance networks. It orbits in Geostationary Orbit (GEO) at altitudes between 36,084 km and 36,087 km with an inclination of 6.9°. It travels at approximately 11,031 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 INSAT 4CR 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 4CR 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 6.9°, 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 4CR’s average altitude, there are currently 148 active payloads and 11 tracked debris or rocket body fragments. India operates approximately 108 active satellites in total, of which 5 share a similar altitude band with INSAT 4CR.
❓ Frequently Asked Questions
INSAT 4CR orbits at approximately 36,086 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 11,031 km/h — it just keeps pace with the ground below. With an inclination of 6.9°, it actually traces a small figure-of-eight pattern rather than remaining perfectly fixed. Learn more about geostationary orbits.
INSAT 4CR is operated by India. It is catalogued by the U.S. Space Surveillance Network under NORAD ID 32050. You can track INSAT 4CR in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
INSAT 4CR was launched on 2007-09-02 from SRI. View the full satellite launch log.
Yes — Orbital Radar tracks INSAT 4CR (NORAD ID 32050) 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 4CR travels at approximately 11,031 km/h (6,854 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.