IRNSS 1I
NORAD 43286
Payload
GEO
2018-035A
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GEO · NORAD 43286
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Altitude (km)
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Speed (km/s)
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Latitude
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Longitude
🛰️ Orbital Parameters
Perigee
35711 km
Apogee
35862 km
Inclination
28.8°
Period
1436.1 min
Mean Motion
1.00272046 rev/day
TLE Epoch
2026-06-15 20:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude35,787 km
Orbital Velocity11,070 km/h
Velocity3.07 km/s
Orbital Period~24 hours (geosynchronous)
Orbits / Day1.00
Eccentricity0.0018
Semi-Major Axis42,158 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
🇮🇳 Indian Space Research Organization (ISRO) (India)
Launch Date
2018-04-11
Launch Site
SRI
Int'l Designator
2018-035A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
IRNSS 1I is an active satellite operated by Indian Space Research Organization (ISRO) (India), launched on 2018-04-11 from SRI. It orbits in Geostationary Orbit (GEO) at altitudes between 35,711 km and 35,862 km with an inclination of 28.8°. 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 1I 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 1I 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 28.8°, 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 1I’s average altitude, there are currently 713 active payloads and 59 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 1I.
❓ Frequently Asked Questions
IRNSS 1I orbits at approximately 35,787 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 28.8°, it actually traces a small figure-of-eight pattern rather than remaining perfectly fixed. Learn more about geostationary orbits.
IRNSS 1I is operated by Indian Space Research Organization (ISRO) (India). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 43286. You can track IRNSS 1I in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
IRNSS 1I was launched on 2018-04-11 from SRI. View the full satellite launch log.
Yes — Orbital Radar tracks IRNSS 1I (NORAD ID 43286) 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 1I 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.