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DELTA 4 R/B

NORAD 37754 Rocket Body MEO 2011-036B
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Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
20129 km
Apogee
22149 km
Inclination
57.0°
Period
757.1 min
Mean Motion
1.90191845 rev/day
TLE Epoch
2026-06-24 14:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude21,139 km
Orbital Velocity13,703 km/h
Velocity3.81 km/s
Orbital Period12 hours 37 minutes
Orbits / Day1.90
Eccentricity0.0367
Semi-Major Axis27,510 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
2011-07-16
Launch Site
Cape Canaveral, Florida
Int'l Designator
2011-036B
Object Type
Rocket Body
RCS Size
Large (>1 m²)
📖 About This Object
DELTA 4 R/B is a spent rocket body associated with United States, launched on 2011-07-16 from Cape Canaveral, Florida on the GPS SVN 63 launch. After 15 years in orbit, it continues to be tracked by global surveillance networks. It orbits in Medium Earth Orbit (MEO) at altitudes between 20,129 km and 22,149 km with an inclination of 57.0°. It travels at approximately 13,703 km/h (3.81 km/s), completing one full orbit every 12 hours 37 minutes — that’s roughly 1.90 orbits per day. Spent rocket bodies like DELTA 4 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
DELTA 4 R/B orbits at an average altitude of 21,139 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 DELTA 4 R/B’s average altitude, there are currently 0 active payloads and 21 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 57.0°, DELTA 4 R/B passes over latitudes between 57.0°N and 57.0°S, covering most populated land masses in both hemispheres. This mid-inclination band balances global coverage with efficient launch energy requirements. 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
DELTA 4 R/B orbits in Medium Earth Orbit (MEO) at altitudes between 20,129 km (perigee) and 22,149 km (apogee), with an average altitude of approximately 21,139 km. It completes one orbit every 12 hours 37 minutes, travelling at approximately 13,703 km/h (8,515 mph).
DELTA 4 R/B (NORAD ID 37754) 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.
DELTA 4 R/B was launched on 2011-07-16 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 DELTA 4 R/B (NORAD ID 37754) 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.
DELTA 4 R/B travels at approximately 13,703 km/h (8,515 mph) — roughly 3.81 km/s. It completes 1.90 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 4 sunrises and sunsets every 24 hours.