INDOSTAR 1
NORAD 25050
Payload
GEO
1997-071B
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GEO · NORAD 25050
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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
35763 km
Apogee
35784 km
Inclination
13.0°
Period
1435.4 min
Mean Motion
1.00318905 rev/day
TLE Epoch
2026-06-17 16:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude35,774 km
Orbital Velocity11,071 km/h
Velocity3.08 km/s
Orbital Period~24 hours (geosynchronous)
Orbits / Day1.00
Eccentricity0.0002
Semi-Major Axis42,145 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
Indonesia
Launch Date
1997-11-11
Launch Site
Guiana Space Centre, Kourou
Int'l Designator
1997-071B
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
INDOSTAR 1 is an active satellite operated by Indonesia, launched on 1997-11-11 from Guiana Space Centre, Kourou. With over 29 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Geostationary Orbit (GEO) at altitudes between 35,763 km and 35,784 km with an inclination of 13.0°. It travels at approximately 11,071 km/h (3.08 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 INDOSTAR 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
INDOSTAR 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 13.0°, 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 INDOSTAR 1’s average altitude, there are currently 707 active payloads and 56 tracked debris or rocket body fragments — notable neighbours include ASTRA 1N, GOES 16, TDRS 13. Indonesia operates approximately 17 active satellites in total, of which 10 share a similar altitude band with INDOSTAR 1.
❓ Frequently Asked Questions
INDOSTAR 1 orbits at approximately 35,774 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 11,071 km/h — it just keeps pace with the ground below. With an inclination of 13.0°, it actually traces a small figure-of-eight pattern rather than remaining perfectly fixed. Learn more about geostationary orbits.
INDOSTAR 1 is operated by Indonesia. It is catalogued by the U.S. Space Surveillance Network under NORAD ID 25050. You can track INDOSTAR 1 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
INDOSTAR 1 was launched on 1997-11-11 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 INDOSTAR 1 (NORAD ID 25050) 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.
INDOSTAR 1 travels at approximately 11,071 km/h (6,879 mph) — roughly 3.08 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.