Skip to content
Home Library Satellite Directory VANGUARD R/B

VANGUARD R/B

NORAD 16 Rocket Body MEO 1958-002A
CONNECTING… MEO · NORAD 16
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
657 km
Apogee
4210 km
Inclination
34.3°
Period
137.2 min
Mean Motion
10.49622701 rev/day
TLE Epoch
2026-09-15 18:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude2,434 km
Orbital Velocity24,223 km/h
Velocity6.73 km/s
Orbital Period2 hours 17 minutes
Orbits / Day10.50
Eccentricity0.2018
Semi-Major Axis8,805 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
1958-03-17
Launch Site
Cape Canaveral Space Force Station, United States
Int'l Designator
1958-002A
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 1958-03-17 from Cape Canaveral Space Force Station, United States. After more than 68 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 657 km and 4,210 km with an inclination of 34.3°. It travels at approximately 24,223 km/h (6.73 km/s), completing one full orbit every 2 hours 17 minutes — that’s roughly 10.50 orbits per day. Its orbital eccentricity of 0.2018 gives it a noticeably elliptical path, with significant altitude variation between perigee and apogee. 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 2,434 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 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 34.3°, VANGUARD R/B passes over latitudes between 34.3°N and 34.3°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 657 km (perigee) and 4,210 km (apogee), with an average altitude of approximately 2,434 km. It completes one orbit every 2 hours 17 minutes, travelling at approximately 24,223 km/h (15,051 mph).
VANGUARD R/B (NORAD ID 16) 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 1958-03-17 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: effectively permanent — above atmospheric drag. View the full satellite launch log.
Yes — Orbital Radar tracks VANGUARD R/B (NORAD ID 16) 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 24,223 km/h (15,051 mph) — roughly 6.73 km/s. It completes 10.50 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 21 sunrises and sunsets every 24 hours.