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DELTA 1 R/B

NORAD 6237 Rocket Body LEO 1972-082C
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Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
916 km
Apogee
1463 km
Inclination
102.8°
Period
109.2 min
Mean Motion
13.18721962 rev/day
TLE Epoch
2026-09-16 00:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude1,190 km
Orbital Velocity26,139 km/h
Velocity7.26 km/s
Orbital Period109 minutes
Orbits / Day13.19
Eccentricity0.0362
Semi-Major Axis7,561 km
Est. Orbital Lifetime~500–1,000 years
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
1972-10-15
Launch Site
Vandenberg Space Force Base, United States
Int'l Designator
1972-082C
Object Type
Rocket Body
RCS Size
Large (>1 m²)
📖 About This Object
DELTA 1 R/B is a spent rocket body associated with United States, launched on 1972-10-15 from Vandenberg Space Force Base, United States on the ITOS D launch. After more than 54 years in orbit, it is one of the longest-surviving objects in the space catalogue. It orbits in Low Earth Orbit (LEO) at altitudes between 916 km and 1,463 km with an inclination of 102.8°. It travels at approximately 26,139 km/h (7.26 km/s), completing one full orbit every 109 minutes — that’s roughly 13.19 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~500–1,000 years. 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 1,190 km in the upper LEO band, where atmospheric drag is negligible and objects can persist for centuries to millennia. This altitude is used by broadband constellations like OneWeb and by scientific missions requiring stable orbits far from the densest debris bands. Within ±50 km of DELTA 1 R/B’s average altitude, there are currently 869 active payloads and 294 tracked debris or rocket body fragments — notable neighbours include ONEWEB-0012, ONEWEB-0010, ONEWEB-0008. With an inclination of 102.8°, DELTA 1 R/B passes over latitudes between 102.8°N and 102.8°S, providing near-global coverage including the polar regions. Polar and near-polar orbits are used for reconnaissance, weather monitoring and Earth-observation missions that need to image every part of the planet. United States operates approximately 13,206 active satellites in total, of which 7 share a similar altitude band with DELTA 1 R/B.
🔗 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 Low Earth Orbit (LEO) at altitudes between 916 km (perigee) and 1,463 km (apogee), with an average altitude of approximately 1,190 km. It completes one orbit every 109 minutes, travelling at approximately 26,139 km/h (16,242 mph).
DELTA 1 R/B (NORAD ID 6237) 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 1972-10-15 from Vandenberg Space Force Base, United States, primarily used for polar and sun-synchronous orbit launches due to its southward ocean trajectory from California. At its current altitude, the estimated remaining orbital lifetime is: ~500–1,000 years. View the full satellite launch log.
Yes — Orbital Radar tracks DELTA 1 R/B (NORAD ID 6237) 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 26,139 km/h (16,242 mph) — roughly 7.26 km/s. It completes 13.19 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 26 sunrises and sunsets every 24 hours.