IABS R/B
NORAD 21877
Rocket Body
MEO
1992-006C
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MEO · NORAD 21877
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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
30472 km
Apogee
35676 km
Inclination
7.5°
Period
1299.8 min
Mean Motion
1.10787098 rev/day
TLE Epoch
2026-06-26 03:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude33,074 km
Orbital Velocity11,444 km/h
Velocity3.18 km/s
Orbital Period21 hours 40 minutes
Orbits / Day1.11
Eccentricity0.0660
Semi-Major Axis39,445 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
1992-02-11
Launch Site
Cape Canaveral, Florida
Int'l Designator
1992-006C
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 1992-02-11 from Cape Canaveral, Florida on the DSCS III B-14 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 30,472 km and 35,676 km with an inclination of 7.5°. It travels at approximately 11,444 km/h (3.18 km/s), completing one full orbit every 21 hours 40 minutes — that’s roughly 1.11 orbits per day. 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 orbits at an average altitude of 33,074 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. With an inclination of 7.5°, IABS R/B passes over latitudes between 7.5°N and 7.5°S, concentrating coverage over equatorial and near-equatorial regions. Low-inclination orbits maximise revisit rates over specific tropical zones. 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 in Medium Earth Orbit (MEO) at altitudes between 30,472 km (perigee) and 35,676 km (apogee), with an average altitude of approximately 33,074 km. It completes one orbit every 21 hours 40 minutes, travelling at approximately 11,444 km/h (7,111 mph).
IABS R/B (NORAD ID 21877) 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 1992-02-11 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 21877) 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 11,444 km/h (7,111 mph) — roughly 3.18 km/s. It completes 1.11 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 2 sunrises and sunsets every 24 hours.