OPTUS B1 R/B(STAR 63F)
NORAD 22089
Rocket Body
MEO
1992-054C
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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
464 km
Apogee
36040 km
Inclination
22.9°
Period
641.1 min
Mean Motion
2.24596320 rev/day
TLE Epoch
2026-06-25 20:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude18,252 km
Orbital Velocity14,484 km/h
Velocity4.02 km/s
Orbital Period10 hours 41 minutes
Orbits / Day2.25
Eccentricity0.7224
Semi-Major Axis24,623 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇦🇺 Optus (Australia)
Launch Date
1992-08-13
Launch Site
Xichang, China
Int'l Designator
1992-054C
Object Type
Rocket Body
RCS Size
Large (>1 m²)
📖 About This Object
OPTUS B1 R/B(STAR 63F) is a spent rocket body associated with Australia, launched on 1992-08-13 from Xichang, China on the Optus B1 launch. With over 34 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Medium Earth Orbit (MEO) at altitudes between 464 km and 36,040 km with an inclination of 22.9°. It travels at approximately 14,484 km/h (4.02 km/s), completing one full orbit every 10 hours 41 minutes — that’s roughly 2.25 orbits per day. Its orbital eccentricity of 0.7224 gives it a noticeably elliptical path, with significant altitude variation between perigee and apogee. Spent rocket bodies like OPTUS B1 R/B(STAR 63F) are among the largest pieces of uncontrolled space debris and are priority targets for collision avoidance manoeuvres and future active debris removal efforts.
🌍 Orbit Context
OPTUS B1 R/B(STAR 63F) orbits at an average altitude of 18,252 km in Medium Earth Orbit, the region between LEO and GEO (2,000–35,786 km). MEO’s higher altitude gives each satellite a much larger ground footprint than LEO, meaning fewer spacecraft are needed for global coverage — but signal latency is higher and radiation from the Van Allen belts is a significant design constraint. Within ±50 km of OPTUS B1 R/B(STAR 63F)’s average altitude, there are currently 1 active payload and 36 tracked debris or rocket body fragments. This is a relatively sparse altitude band, containing less than 1% of all active satellites. With an inclination of 22.9°, OPTUS B1 R/B(STAR 63F) passes over latitudes between 22.9°N and 22.9°S, covering the tropical and temperate zones where most of the world’s population resides. Low-to-mid inclination orbits are efficient to reach from equatorial and mid-latitude launch sites. Australia operates approximately 41 active satellites in total.
🔗 Spent Rocket Body
This is a spent rocket body — the upper stage of a launch vehicle that remains in orbit after delivering its payload. Rocket bodies are a significant contributor to the space debris population. Older stages often retained residual propellant that could later explode, creating debris fields. Modern guidelines require upper stages to either deorbit (controlled re-entry) or passivate (vent residual fuel) to reduce fragmentation risk. The FCC's 5-year deorbit rule and UN debris mitigation guidelines are increasingly enforced to address this growing problem.
❓ Frequently Asked Questions
OPTUS B1 R/B(STAR 63F) orbits in Medium Earth Orbit (MEO) at altitudes between 464 km (perigee) and 36,040 km (apogee), with an average altitude of approximately 18,252 km. It completes one orbit every 10 hours 41 minutes, travelling at approximately 14,484 km/h (9,000 mph).
OPTUS B1 R/B(STAR 63F) (NORAD ID 22089) is a spent rocket body — the upper stage of a launch vehicle attributed to Australia. It no longer serves a functional purpose but continues to orbit Earth as tracked debris. Spent upper stages are among the largest uncontrolled objects in orbit and are closely monitored for collision risk.
OPTUS B1 R/B(STAR 63F) was launched on 1992-08-13 from Xichang, China. At its current altitude, the estimated remaining orbital lifetime is: effectively permanent — above atmospheric drag. View the full satellite launch log.
Yes — Orbital Radar tracks OPTUS B1 R/B(STAR 63F) (NORAD ID 22089) 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 B1 R/B(STAR 63F) travels at approximately 14,484 km/h (9,000 mph) — roughly 4.02 km/s. It completes 2.25 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 4 sunrises and sunsets every 24 hours.