DELTA 4 R/B
NORAD 39742
Rocket Body
MEO
2014-026B
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MEO · NORAD 39742
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Altitude (km)
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Longitude
🛰️ Orbital Parameters
Perigee
20749 km
Apogee
20826 km
Inclination
56.6°
Period
742.6 min
Mean Motion
1.93899024 rev/day
TLE Epoch
2026-06-23 12:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude20,788 km
Orbital Velocity13,792 km/h
Velocity3.83 km/s
Orbital Period12 hours 23 minutes
Orbits / Day1.94
Eccentricity0.0014
Semi-Major Axis27,159 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
2014-05-17
Launch Site
Cape Canaveral, Florida
Int'l Designator
2014-026B
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 2014-05-17 from Cape Canaveral, Florida on the GPS SVN 67 launch. After 12 years in orbit, it continues to be tracked by global surveillance networks. It orbits in Medium Earth Orbit (MEO) at altitudes between 20,749 km and 20,826 km with an inclination of 56.6°. It travels at approximately 13,792 km/h (3.83 km/s), completing one full orbit every 12 hours 23 minutes — that’s roughly 1.94 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 20,788 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 1 active payload and 9 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 56.6°, DELTA 4 R/B passes over latitudes between 56.6°N and 56.6°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 20,749 km (perigee) and 20,826 km (apogee), with an average altitude of approximately 20,788 km. It completes one orbit every 12 hours 23 minutes, travelling at approximately 13,792 km/h (8,570 mph).
DELTA 4 R/B (NORAD ID 39742) 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 2014-05-17 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 39742) 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 13,792 km/h (8,570 mph) — roughly 3.83 km/s. It completes 1.94 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 4 sunrises and sunsets every 24 hours.