ATLAS AGENA R/B
NORAD 27785
Rocket Body
MEO
1968-063B
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Longitude
🛰️ Orbital Parameters
Perigee
31132 km
Apogee
39610 km
Inclination
4.4°
Period
1414.9 min
Mean Motion
1.01772935 rev/day
TLE Epoch
2026-06-25 23:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude35,371 km
Orbital Velocity11,125 km/h
Velocity3.09 km/s
Orbital Period23 hours 35 minutes
Orbits / Day1.02
Eccentricity0.1016
Semi-Major Axis41,742 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
1968-08-06
Launch Site
Cape Canaveral, Florida
Int'l Designator
1968-063B
Object Type
Rocket Body
RCS Size
Medium (0.1–1 m²)
📖 About This Object
ATLAS AGENA R/B is a spent rocket body associated with United States, launched on 1968-08-06 from Cape Canaveral, Florida on the CANYON 1 launch. After more than 58 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 31,132 km and 39,610 km with an inclination of 4.4°. It travels at approximately 11,125 km/h (3.09 km/s), completing one full orbit every 23 hours 35 minutes — that’s roughly 1.02 orbits per day. Its orbital eccentricity of 0.1016 gives it a noticeably elliptical path, with significant altitude variation between perigee and apogee. 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 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 R/B orbits at an average altitude of 35,371 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 ATLAS AGENA R/B’s average altitude, there are currently 0 active payloads and 9 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 4.4°, ATLAS AGENA R/B passes over latitudes between 4.4°N and 4.4°S, concentrating coverage over equatorial and near-equatorial regions. Low-inclination orbits maximise revisit rates over specific tropical zones. United States operates approximately 12,413 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
ATLAS AGENA R/B orbits in Medium Earth Orbit (MEO) at altitudes between 31,132 km (perigee) and 39,610 km (apogee), with an average altitude of approximately 35,371 km. It completes one orbit every 23 hours 35 minutes, travelling at approximately 11,125 km/h (6,913 mph).
ATLAS AGENA R/B (NORAD ID 27785) 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 R/B was launched on 1968-08-06 from Cape Canaveral, Florida, 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 R/B (NORAD ID 27785) 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 R/B travels at approximately 11,125 km/h (6,913 mph) — roughly 3.09 km/s. It completes 1.02 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 2 sunrises and sunsets every 24 hours.