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DELTA 1 R/B

NORAD 3616 Rocket Body LEO 1968-114B
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
1448 km
Apogee
1469 km
Inclination
101.7°
Period
115.1 min
Mean Motion
12.51403539 rev/day
TLE Epoch
2026-09-16 06:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude1,459 km
Orbital Velocity25,686 km/h
Velocity7.14 km/s
Orbital Period115 minutes
Orbits / Day12.51
Eccentricity0.0013
Semi-Major Axis7,830 km
Est. Orbital LifetimeThousands of years
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
1968-12-15
Launch Site
Vandenberg Space Force Base, United States
Int'l Designator
1968-114B
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 1968-12-15 from Vandenberg Space Force Base, United States on the TOS F launch. After more than 58 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 1,448 km and 1,469 km with an inclination of 101.7°. It travels at approximately 25,686 km/h (7.14 km/s), completing one full orbit every 115 minutes — that’s roughly 12.51 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is thousands of 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 1,459 km in the uppermost reaches of Low Earth Orbit. At this altitude, orbital decay is effectively zero without active deorbiting, and coverage footprints are significantly larger than lower LEO, though at the cost of higher latency. Within ±50 km of DELTA 1 R/B’s average altitude, there are currently 533 active payloads and 367 tracked debris or rocket body fragments. With an inclination of 101.7°, DELTA 1 R/B passes over latitudes between 101.7°N and 101.7°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 16 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 1,448 km (perigee) and 1,469 km (apogee), with an average altitude of approximately 1,459 km. It completes one orbit every 115 minutes, travelling at approximately 25,686 km/h (15,961 mph).
DELTA 1 R/B (NORAD ID 3616) 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 1968-12-15 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: thousands of years. View the full satellite launch log.
Yes — Orbital Radar tracks DELTA 1 R/B (NORAD ID 3616) 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 25,686 km/h (15,961 mph) — roughly 7.14 km/s. It completes 12.51 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 25 sunrises and sunsets every 24 hours.