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TELKOM 2

NORAD 28902 Payload GEO 2005-046A ● Active
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
36081 km
Apogee
36130 km
Inclination
4.8°
Period
1452.4 min
Mean Motion
0.99144701 rev/day
TLE Epoch
2026-06-19 20:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude36,106 km
Orbital Velocity11,028 km/h
Velocity3.06 km/s
Orbital Period24.2 hours
Orbits / Day0.99
Eccentricity0.0006
Semi-Major Axis42,477 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
Indonesia
Launch Date
2005-11-16
Launch Site
Guiana Space Centre, Kourou
Int'l Designator
2005-046A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
TELKOM 2 is an active satellite operated by Indonesia, launched on 2005-11-16 from Guiana Space Centre, Kourou. With over 21 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Geostationary Orbit (GEO) at altitudes between 36,081 km and 36,130 km with an inclination of 4.8°. It travels at approximately 11,028 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 TELKOM 2 in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
TELKOM 2 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 4.8°, 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 TELKOM 2’s average altitude, there are currently 176 active payloads and 7 tracked debris or rocket body fragments. Indonesia operates approximately 17 active satellites in total, of which 2 share a similar altitude band with TELKOM 2.
❓ Frequently Asked Questions
TELKOM 2 orbits at approximately 36,106 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 11,028 km/h — it just keeps pace with the ground below. With an inclination of 4.8°, it actually traces a small figure-of-eight pattern rather than remaining perfectly fixed. Learn more about geostationary orbits.
TELKOM 2 is operated by Indonesia. It is catalogued by the U.S. Space Surveillance Network under NORAD ID 28902. You can track TELKOM 2 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
TELKOM 2 was launched on 2005-11-16 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 TELKOM 2 (NORAD ID 28902) 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.
TELKOM 2 travels at approximately 11,028 km/h (6,852 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.