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TITAN 34B R/B

NORAD 7688 Rocket Body MEO 1975-017B
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
232 km
Apogee
15093 km
Inclination
63.3°
Period
276.0 min
Mean Motion
5.21876611 rev/day
TLE Epoch
2026-09-16 03:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude7,663 km
Orbital Velocity19,186 km/h
Velocity5.33 km/s
Orbital Period4 hours 36 minutes
Orbits / Day5.22
Eccentricity0.5295
Semi-Major Axis14,034 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
1975-03-10
Launch Site
Vandenberg Space Force Base, United States
Int'l Designator
1975-017B
Object Type
Rocket Body
RCS Size
Large (>1 m²)
📖 About This Object
TITAN 34B R/B is a spent rocket body associated with United States, launched on 1975-03-10 from Vandenberg Space Force Base, United States on the Jumpseat 4 launch. After more than 51 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 232 km and 15,093 km with an inclination of 63.3°. It travels at approximately 19,186 km/h (5.33 km/s), completing one full orbit every 4 hours 36 minutes — that’s roughly 5.22 orbits per day. Its orbital eccentricity of 0.5295 gives it a noticeably elliptical path, with significant altitude variation between perigee and apogee. Spent rocket bodies like TITAN 34B 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
TITAN 34B R/B orbits at an average altitude of 7,663 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 TITAN 34B R/B’s average altitude, there are currently 0 active payloads and 12 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 63.3°, TITAN 34B R/B passes over latitudes between 63.3°N and 63.3°S, covering most populated land masses in both hemispheres. This mid-inclination band balances global coverage with efficient launch energy requirements. 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
TITAN 34B R/B orbits in Medium Earth Orbit (MEO) at altitudes between 232 km (perigee) and 15,093 km (apogee), with an average altitude of approximately 7,663 km. It completes one orbit every 4 hours 36 minutes, travelling at approximately 19,186 km/h (11,922 mph).
TITAN 34B R/B (NORAD ID 7688) 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.
TITAN 34B R/B was launched on 1975-03-10 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: effectively permanent — above atmospheric drag. View the full satellite launch log.
Yes — Orbital Radar tracks TITAN 34B R/B (NORAD ID 7688) 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.
TITAN 34B R/B travels at approximately 19,186 km/h (11,922 mph) — roughly 5.33 km/s. It completes 5.22 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 10 sunrises and sunsets every 24 hours.