IABS R/B
NORAD 26577
Rocket Body
GEO
2000-065C
CONNECTING…
GEO · NORAD 26577
NOW PASSING OVER
Calculating position…
—
Altitude (km)
—
Speed (km/s)
—
Latitude
—
Longitude
🛰️ Orbital Parameters
Perigee
35301 km
Apogee
35768 km
Inclination
14.0°
Period
1423.2 min
Mean Motion
1.01178412 rev/day
TLE Epoch
2026-06-25 06:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude35,535 km
Orbital Velocity11,103 km/h
Velocity3.08 km/s
Orbital Period23 hours 43 minutes
Orbits / Day1.01
Eccentricity0.0056
Semi-Major Axis41,906 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
2000-10-20
Launch Site
Cape Canaveral, Florida
Int'l Designator
2000-065C
Object Type
Rocket Body
RCS Size
Medium (0.1–1 m²)
📖 About This Object
IABS R/B is a spent rocket body associated with United States, launched on 2000-10-20 from Cape Canaveral, Florida on the DSCS III B-11 launch. With over 26 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Geostationary Orbit (GEO) at altitudes between 35,301 km and 35,768 km with an inclination of 14.0°. It travels at approximately 11,103 km/h (3.08 km/s), completing one full orbit every 23 hours 43 minutes — that’s roughly 1.01 orbits per day. At geostationary altitude, there is no meaningful atmospheric drag — this object will remain in orbit indefinitely unless actively deorbited. Spent rocket bodies like IABS R/B 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
IABS R/B 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 14.0°, 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 IABS R/B’s average altitude, there are currently 1 active payload and 38 tracked debris or rocket body fragments. United States operates approximately 12,413 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
IABS R/B orbits at approximately 35,535 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 11,103 km/h — it just keeps pace with the ground below. With an inclination of 14.0°, it actually traces a small figure-of-eight pattern rather than remaining perfectly fixed. Learn more about geostationary orbits.
IABS R/B (NORAD ID 26577) is a spent rocket body — the upper stage of a launch vehicle attributed to United States. 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.
IABS R/B was launched on 2000-10-20 from Cape Canaveral, Florida, one of the busiest launch facilities in the world, operated by NASA and the U.S. Space Force on Florida’s Atlantic coast. View the full satellite launch log.
Yes — Orbital Radar tracks IABS R/B (NORAD ID 26577) 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.
IABS R/B travels at approximately 11,103 km/h (6,899 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.