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DELTA 1 R/B

NORAD 50 Rocket Body LEO 1960-009B
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
1501 km
Apogee
1683 km
Inclination
47.2°
Period
118.0 min
Mean Motion
12.20169523 rev/day
TLE Epoch
2026-09-16 00:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude1,592 km
Orbital Velocity25,470 km/h
Velocity7.08 km/s
Orbital Period118 minutes
Orbits / Day12.20
Eccentricity0.0114
Semi-Major Axis7,963 km
Est. Orbital LifetimeThousands of years
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
1960-08-12
Launch Site
Cape Canaveral Space Force Station, United States
Int'l Designator
1960-009B
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 1960-08-12 from Cape Canaveral Space Force Station, United States. After more than 66 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 1,501 km and 1,683 km with an inclination of 47.2°. It travels at approximately 25,470 km/h (7.08 km/s), completing one full orbit every 118 minutes — that’s roughly 12.20 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 1,592 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 37 active payloads and 286 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 47.2°, DELTA 1 R/B passes over latitudes between 47.2°N and 47.2°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, of which 3 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 1,501 km (perigee) and 1,683 km (apogee), with an average altitude of approximately 1,592 km. It completes one orbit every 118 minutes, travelling at approximately 25,470 km/h (15,826 mph).
DELTA 1 R/B (NORAD ID 50) 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 1960-08-12 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: thousands of years. View the full satellite launch log.
Yes — Orbital Radar tracks DELTA 1 R/B (NORAD ID 50) 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 25,470 km/h (15,826 mph) — roughly 7.08 km/s. It completes 12.20 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 24 sunrises and sunsets every 24 hours.