Skip to content
Home Library Satellite Directory VANGUARD R/B

VANGUARD R/B

NORAD 12 Rocket Body MEO 1959-001B
CONNECTING… MEO · NORAD 12
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
554 km
Apogee
3284 km
Inclination
32.9°
Period
125.4 min
Mean Motion
11.48648000 rev/day
TLE Epoch
2026-09-16 00:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude1,919 km
Orbital Velocity24,963 km/h
Velocity6.93 km/s
Orbital Period2 hours 5 minutes
Orbits / Day11.49
Eccentricity0.1647
Semi-Major Axis8,290 km
Est. Orbital LifetimeThousands of years
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
1959-02-17
Launch Site
Cape Canaveral Space Force Station, United States
Int'l Designator
1959-001B
Object Type
Rocket Body
RCS Size
Medium (0.1–1 m²)
📖 About This Object
VANGUARD R/B is a spent rocket body associated with United States, launched on 1959-02-17 from Cape Canaveral Space Force Station, United States. After more than 67 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 554 km and 3,284 km with an inclination of 32.9°. It travels at approximately 24,963 km/h (6.93 km/s), completing one full orbit every 2 hours 5 minutes — that’s roughly 11.49 orbits per day. Its orbital eccentricity of 0.1647 gives it a noticeably elliptical path, with significant altitude variation between perigee and apogee. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is thousands of years. Spent rocket bodies like VANGUARD 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
VANGUARD R/B orbits at an average altitude of 1,919 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 VANGUARD R/B’s average altitude, there are currently 5 active payloads and 27 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 32.9°, VANGUARD R/B passes over latitudes between 32.9°N and 32.9°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.
🔗 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
VANGUARD R/B orbits in Medium Earth Orbit (MEO) at altitudes between 554 km (perigee) and 3,284 km (apogee), with an average altitude of approximately 1,919 km. It completes one orbit every 2 hours 5 minutes, travelling at approximately 24,963 km/h (15,511 mph).
VANGUARD R/B (NORAD ID 12) 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.
VANGUARD R/B was launched on 1959-02-17 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 VANGUARD R/B (NORAD ID 12) 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.
VANGUARD R/B travels at approximately 24,963 km/h (15,511 mph) — roughly 6.93 km/s. It completes 11.49 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 23 sunrises and sunsets every 24 hours.