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IRNSS 1F

NORAD 41384 Payload GEO 2016-015A ● Active
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
35714 km
Apogee
35861 km
Inclination
5.3°
Period
1436.2 min
Mean Motion
1.00268295 rev/day
TLE Epoch
2026-06-18 23:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude35,788 km
Orbital Velocity11,070 km/h
Velocity3.07 km/s
Orbital Period~24 hours (geosynchronous)
Orbits / Day1.00
Eccentricity0.0017
Semi-Major Axis42,159 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
🇮🇳 Indian Space Research Organization (ISRO) (India)
Launch Date
2016-03-10
Launch Site
SRI
Int'l Designator
2016-015A
Object Type
Payload
RCS Size
Medium (0.1–1 m²)
📖 About This Object
IRNSS 1F is an active satellite operated by Indian Space Research Organization (ISRO) (India), launched on 2016-03-10 from SRI. After 10 years in orbit, it continues to be tracked by global surveillance networks. It orbits in Geostationary Orbit (GEO) at altitudes between 35,714 km and 35,861 km with an inclination of 5.3°. It travels at approximately 11,070 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 IRNSS 1F in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
IRNSS 1F 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 5.3°, 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 IRNSS 1F’s average altitude, there are currently 714 active payloads and 60 tracked debris or rocket body fragments — notable neighbours include ASTRA 1N, GOES 16, TDRS 13. India operates approximately 108 active satellites in total, of which 36 share a similar altitude band with IRNSS 1F.
❓ Frequently Asked Questions
IRNSS 1F orbits at approximately 35,788 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 11,070 km/h — it just keeps pace with the ground below. With an inclination of 5.3°, it actually traces a small figure-of-eight pattern rather than remaining perfectly fixed. Learn more about geostationary orbits.
IRNSS 1F is operated by Indian Space Research Organization (ISRO) (India). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 41384. You can track IRNSS 1F in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
IRNSS 1F was launched on 2016-03-10 from SRI. View the full satellite launch log.
Yes — Orbital Radar tracks IRNSS 1F (NORAD ID 41384) 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.
IRNSS 1F travels at approximately 11,070 km/h (6,878 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.