ATLAS AGENA D R/B
NORAD 4511
Rocket Body
GEO
1970-046B
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GEO · NORAD 4511
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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
35610 km
Apogee
35869 km
Inclination
1.9°
Period
1433.7 min
Mean Motion
1.00440502 rev/day
TLE Epoch
2026-09-15 14:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude35,740 km
Orbital Velocity11,076 km/h
Velocity3.08 km/s
Orbital Period~24 hours (geosynchronous)
Orbits / Day1.00
Eccentricity0.0031
Semi-Major Axis42,111 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
1970-06-19
Launch Site
Cape Canaveral Space Force Station, United States
Int'l Designator
1970-046B
Object Type
Rocket Body
RCS Size
Medium (0.1–1 m²)
📖 About This Object
ATLAS AGENA D R/B is a spent rocket body associated with United States, launched on 1970-06-19 from Cape Canaveral Space Force Station, United States on the RHYOLITE 1 launch. After more than 56 years in orbit, it is one of the longest-surviving objects in the space catalogue. It orbits in Geostationary Orbit (GEO) at altitudes between 35,610 km and 35,869 km with an inclination of 1.9°. It travels at approximately 11,076 km/h (3.08 km/s), completing one full orbit every ~24 hours (geosynchronous) — that’s roughly 1.00 orbits per day. At geostationary altitude, there is no meaningful atmospheric drag — this object will remain in orbit indefinitely unless actively deorbited. Spent rocket bodies like ATLAS AGENA D 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
ATLAS AGENA D R/B occupies geostationary orbit at approximately 35,786 km above the equator, where its orbital period matches the Earth’s 24-hour rotation. From the ground, it appears to hover over a fixed point — ideal for broadcast television, weather monitoring and wideband communications. With an inclination of 1.9°, it traces a small figure-of-eight pattern relative to the equator rather than remaining perfectly stationary, which can indicate aging stationkeeping fuel or a deliberate inclined-orbit strategy. Within ±50 km of ATLAS AGENA D R/B’s average altitude, there are currently 661 active payloads and 41 tracked debris or rocket body fragments — notable neighbours include ASTRA 1N, GOES 16, TDRS 13. United States operates approximately 13,206 active satellites in total, of which 142 share a similar altitude band with ATLAS AGENA D 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
ATLAS AGENA D R/B orbits at approximately 35,740 km altitude, where the orbital period matches the Earth’s 24-hour rotation. This means it stays above the same point on the equator at all times. Its actual speed is still 11,076 km/h — it just keeps pace with the ground below. With an inclination of 1.9°, it actually traces a small figure-of-eight pattern rather than remaining perfectly fixed. Learn more about geostationary orbits.
ATLAS AGENA D R/B (NORAD ID 4511) 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.
ATLAS AGENA D R/B was launched on 1970-06-19 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. View the full satellite launch log.
Yes — Orbital Radar tracks ATLAS AGENA D R/B (NORAD ID 4511) 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.
ATLAS AGENA D R/B travels at approximately 11,076 km/h (6,882 mph) — roughly 3.08 km/s. Despite this high speed, it appears stationary from the ground because it matches the Earth’s rotation. Geostationary satellites are actually slower than LEO satellites because orbital velocity decreases with altitude.