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OPTUS C1

NORAD 27831 Payload GEO 2003-028B ● Active
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
35763 km
Apogee
35810 km
Inclination
6.9°
Period
1436.1 min
Mean Motion
1.00272247 rev/day
TLE Epoch
2026-06-19 13:00:00 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
Eccentricity0.0006
Semi-Major Axis42,158 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
🇦🇺 Optus Communications (Parent: Singapore Telecom)/Australian Ministry of Defense (Australia)
Launch Date
2003-06-11
Launch Site
Guiana Space Centre, Kourou
Int'l Designator
2003-028B
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
OPTUS C1 is an active satellite operated by Optus Communications (Parent: Singapore Telecom)/Australian Ministry of Defense (Australia), launched on 2003-06-11 from Guiana Space Centre, Kourou. With over 23 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Geostationary Orbit (GEO) at altitudes between 35,763 km and 35,810 km with an inclination of 6.9°. 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 OPTUS C1 in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
OPTUS C1 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 OPTUS C1’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. Australia operates approximately 41 active satellites in total, of which 7 share a similar altitude band with OPTUS C1.
❓ Frequently Asked Questions
OPTUS C1 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 6.9°, it actually traces a small figure-of-eight pattern rather than remaining perfectly fixed. Learn more about geostationary orbits.
OPTUS C1 is operated by Optus Communications (Parent: Singapore Telecom)/Australian Ministry of Defense (Australia). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 27831. You can track OPTUS C1 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
OPTUS C1 was launched on 2003-06-11 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 OPTUS C1 (NORAD ID 27831) 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.
OPTUS C1 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.