DELTA 1 R/B
NORAD 738
Rocket Body
MEO
1964-003B
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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
1856 km
Apogee
7649 km
Inclination
46.5°
Period
194.8 min
Mean Motion
7.39333511 rev/day
TLE Epoch
2026-09-15 17:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude4,753 km
Orbital Velocity21,550 km/h
Velocity5.99 km/s
Orbital Period3 hours 15 minutes
Orbits / Day7.39
Eccentricity0.2604
Semi-Major Axis11,124 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
1964-01-21
Launch Site
Cape Canaveral Space Force Station, United States
Int'l Designator
1964-003B
Object Type
Rocket Body
RCS Size
Medium (0.1–1 m²)
📖 About This Object
DELTA 1 R/B is a spent rocket body associated with United States, launched on 1964-01-21 from Cape Canaveral Space Force Station, United States on the Relay B launch. After more than 62 years in orbit, it is one of the longest-surviving objects in the space catalogue. It orbits in Medium Earth Orbit (MEO) at altitudes between 1,856 km and 7,649 km with an inclination of 46.5°. It travels at approximately 21,550 km/h (5.99 km/s), completing one full orbit every 3 hours 15 minutes — that’s roughly 7.39 orbits per day. Its orbital eccentricity of 0.2604 gives it a noticeably elliptical path, with significant altitude variation between perigee and apogee. Spent rocket bodies like DELTA 1 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 1 R/B orbits at an average altitude of 4,753 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 1 R/B’s average altitude, there are currently 1 active payload and 6 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 46.5°, DELTA 1 R/B passes over latitudes between 46.5°N and 46.5°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. United States operates approximately 13,206 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 1 R/B orbits in Medium Earth Orbit (MEO) at altitudes between 1,856 km (perigee) and 7,649 km (apogee), with an average altitude of approximately 4,753 km. It completes one orbit every 3 hours 15 minutes, travelling at approximately 21,550 km/h (13,391 mph).
DELTA 1 R/B (NORAD ID 738) 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 1 R/B was launched on 1964-01-21 from Cape Canaveral Space Force Station, United States, one of the busiest launch facilities in the world, operated by NASA and the U.S. Space Force on Florida’s Atlantic coast. 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 DELTA 1 R/B (NORAD ID 738) 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 1 R/B travels at approximately 21,550 km/h (13,391 mph) — roughly 5.99 km/s. It completes 7.39 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 15 sunrises and sunsets every 24 hours.