SCOUT G-1 R/B
NORAD 14155
Rocket Body
LEO
1983-063B
CONNECTING…
LEO · NORAD 14155
NOW PASSING OVER
Calculating position…
—
Altitude (km)
—
Speed (km/s)
—
Latitude
—
Longitude
🛰️ Orbital Parameters
Perigee
719 km
Apogee
773 km
Inclination
82.0°
Period
99.7 min
Mean Motion
14.43776539 rev/day
TLE Epoch
2026-06-25 21:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude746 km
Orbital Velocity26,942 km/h
Velocity7.48 km/s
Orbital Period100 minutes
Orbits / Day14.44
Eccentricity0.0038
Semi-Major Axis7,117 km
Est. Orbital Lifetime~25–100 years
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
1983-06-27
Launch Site
Vandenberg SFB, California
Int'l Designator
1983-063B
Object Type
Rocket Body
RCS Size
Medium (0.1–1 m²)
📖 About This Object
SCOUT G-1 R/B is a spent rocket body associated with United States, launched on 1983-06-27 from Vandenberg SFB, California on the NNS O-16 launch. With over 43 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Low Earth Orbit (LEO) at altitudes between 719 km and 773 km with an inclination of 82.0°. It travels at approximately 26,942 km/h (7.48 km/s), completing one full orbit every 100 minutes — that’s roughly 14.44 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~25–100 years. Spent rocket bodies like SCOUT G-1 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
SCOUT G-1 R/B orbits at an average altitude of 746 km in the mid-LEO band, where atmospheric drag is minimal but radiation exposure remains manageable. Objects at this altitude persist for decades to centuries, making debris mitigation critical. This regime is popular for remote sensing constellations and scientific instruments that need stable, long-duration orbits. Within ±50 km of SCOUT G-1 R/B’s average altitude, there are currently 375 active payloads and 1,934 tracked debris or rocket body fragments — notable neighbours include LANDSAT 9. With an inclination of 82.0°, SCOUT G-1 R/B passes over latitudes between 82.0°N and 82.0°S, providing near-global coverage including the polar regions. Polar and near-polar orbits are used for reconnaissance, weather monitoring and Earth-observation missions that need to image every part of the planet. United States operates approximately 12,413 active satellites in total, of which 147 share a similar altitude band with SCOUT G-1 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
SCOUT G-1 R/B orbits in Low Earth Orbit (LEO) at altitudes between 719 km (perigee) and 773 km (apogee), with an average altitude of approximately 746 km. It completes one orbit every 100 minutes, travelling at approximately 26,942 km/h (16,741 mph).
SCOUT G-1 R/B (NORAD ID 14155) 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.
SCOUT G-1 R/B was launched on 1983-06-27 from Vandenberg SFB, California, primarily used for polar and sun-synchronous orbit launches due to its southward ocean trajectory from California. At its current altitude, the estimated remaining orbital lifetime is: ~25–100 years. View the full satellite launch log.
Yes — Orbital Radar tracks SCOUT G-1 R/B (NORAD ID 14155) 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.
SCOUT G-1 R/B travels at approximately 26,942 km/h (16,741 mph) — roughly 7.48 km/s. It completes 14.44 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 29 sunrises and sunsets every 24 hours.