THOR ABLESTAR R/B
NORAD 1428
Rocket Body
LEO
1965-048B
CONNECTING…
LEO · NORAD 1428
NOW PASSING OVER
Calculating position…
—
Altitude (km)
—
Speed (km/s)
—
Latitude
—
Longitude
🛰️ Orbital Parameters
Perigee
1021 km
Apogee
1103 km
Inclination
89.9°
Period
106.5 min
Mean Motion
13.52692298 rev/day
TLE Epoch
2026-09-16 01:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude1,062 km
Orbital Velocity26,363 km/h
Velocity7.32 km/s
Orbital Period106 minutes
Orbits / Day13.53
Eccentricity0.0055
Semi-Major Axis7,433 km
Est. Orbital Lifetime~500–1,000 years
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
1965-06-24
Launch Site
Vandenberg Space Force Base, United States
Int'l Designator
1965-048B
Object Type
Rocket Body
RCS Size
Large (>1 m²)
📖 About This Object
THOR ABLESTAR R/B is a spent rocket body associated with United States, launched on 1965-06-24 from Vandenberg Space Force Base, United States on the NNS O-4 launch. After more than 61 years in orbit, it is one of the longest-surviving objects in the space catalogue. It orbits in Low Earth Orbit (LEO) at altitudes between 1,021 km and 1,103 km with an inclination of 89.9°. It travels at approximately 26,363 km/h (7.32 km/s), completing one full orbit every 106 minutes — that’s roughly 13.53 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~500–1,000 years. Spent rocket bodies like THOR ABLESTAR 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
THOR ABLESTAR R/B orbits at an average altitude of 1,062 km in the upper LEO band, where atmospheric drag is negligible and objects can persist for centuries to millennia. This altitude is used by broadband constellations like OneWeb and by scientific missions requiring stable orbits far from the densest debris bands. Within ±50 km of THOR ABLESTAR R/B’s average altitude, there are currently 309 active payloads and 606 tracked debris or rocket body fragments — notable neighbours include ONEWEB-0041. With an inclination of 89.9°, THOR ABLESTAR R/B passes over latitudes between 89.9°N and 89.9°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 13,206 active satellites in total, of which 42 share a similar altitude band with THOR ABLESTAR 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
THOR ABLESTAR R/B orbits in Low Earth Orbit (LEO) at altitudes between 1,021 km (perigee) and 1,103 km (apogee), with an average altitude of approximately 1,062 km. It completes one orbit every 106 minutes, travelling at approximately 26,363 km/h (16,381 mph).
THOR ABLESTAR R/B (NORAD ID 1428) 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.
THOR ABLESTAR R/B was launched on 1965-06-24 from Vandenberg Space Force Base, United States, 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: ~500–1,000 years. View the full satellite launch log.
Yes — Orbital Radar tracks THOR ABLESTAR R/B (NORAD ID 1428) 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.
THOR ABLESTAR R/B travels at approximately 26,363 km/h (16,381 mph) — roughly 7.32 km/s. It completes 13.53 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 27 sunrises and sunsets every 24 hours.