Skip to content
Home Library Satellite Directory ATLAS AGENA R/B

ATLAS AGENA R/B

NORAD 27786 Rocket Body MEO 1969-036B
CONNECTING… MEO · NORAD 27786
NOW PASSING OVER
Calculating position…
Altitude (km)
Speed (km/s)
Latitude
Longitude
Real-time tracking powered by Orbital Radar
ORBITAL RADAR · LIVE GROUND TRACK
🌍 Track on 3D Globe
🛰️ Orbital Parameters
Perigee
30451 km
Apogee
39172 km
Inclination
14.4°
Period
1386.6 min
Mean Motion
1.03853649 rev/day
TLE Epoch
2026-06-25 16:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude34,812 km
Orbital Velocity11,200 km/h
Velocity3.11 km/s
Orbital Period23 hours 7 minutes
Orbits / Day1.04
Eccentricity0.1059
Semi-Major Axis41,183 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
1969-04-13
Launch Site
Cape Canaveral, Florida
Int'l Designator
1969-036B
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 1969-04-13 from Cape Canaveral, Florida on the CANYON 2 launch. After more than 57 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 30,451 km and 39,172 km with an inclination of 14.4°. It travels at approximately 11,200 km/h (3.11 km/s), completing one full orbit every 23 hours 7 minutes — that’s roughly 1.04 orbits per day. Its orbital eccentricity of 0.1059 gives it a noticeably elliptical path, with significant altitude variation between perigee and apogee. 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 34,812 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. With an inclination of 14.4°, ATLAS AGENA R/B passes over latitudes between 14.4°N and 14.4°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 30,451 km (perigee) and 39,172 km (apogee), with an average altitude of approximately 34,812 km. It completes one orbit every 23 hours 7 minutes, travelling at approximately 11,200 km/h (6,959 mph).
ATLAS AGENA R/B (NORAD ID 27786) 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 1969-04-13 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 27786) 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 11,200 km/h (6,959 mph) — roughly 3.11 km/s. It completes 1.04 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 2 sunrises and sunsets every 24 hours.