TITAN 3C TRANSTAGE R/B
NORAD 3956
Rocket Body
HEO
1969-046F
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HEO · NORAD 3956
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Altitude (km)
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Speed (km/s)
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Latitude
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Longitude
🛰️ Orbital Parameters
Perigee
7720 km
Apogee
120890 km
Inclination
17.6°
Period
3117.0 min
Mean Motion
0.46197675 rev/day
TLE Epoch
2026-09-17 13:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude64,305 km
Orbital Velocity8,549 km/h
Velocity2.37 km/s
Orbital Period51.9 hours
Orbits / Day0.46
Eccentricity0.8006
Semi-Major Axis70,676 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
1969-05-23
Launch Site
Cape Canaveral Space Force Station, United States
Int'l Designator
1969-046F
Object Type
Rocket Body
RCS Size
Large (>1 m²)
📖 About This Object
TITAN 3C TRANSTAGE R/B is a spent rocket body associated with United States, launched on 1969-05-23 from Cape Canaveral Space Force Station, United States on the ERS 29 launch. After more than 57 years in orbit, it is one of the longest-surviving objects in the space catalogue. It orbits in Highly Elliptical Orbit (HEO) at altitudes between 7,720 km and 120,890 km with an inclination of 17.6°. It travels at approximately 8,549 km/h (2.37 km/s), completing one full orbit every 51.9 hours — that’s roughly 0.46 orbits per day. Its orbital eccentricity of 0.8006 gives it a noticeably elliptical path, with significant altitude variation between perigee and apogee. At geostationary altitude, there is no meaningful atmospheric drag — this object will remain in orbit indefinitely unless actively deorbited. Spent rocket bodies like TITAN 3C TRANSTAGE 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 3C TRANSTAGE R/B follows a Highly Elliptical Orbit, sweeping between 7,720 km (perigee) and 120,890 km (apogee). It spends most of its 51.9 hours orbital period near apogee, effectively loitering over a region of interest before rapidly sweeping through perigee — a profile used for high-latitude communications (Molniya orbits), early-warning systems and magnetospheric science. With an inclination of 17.6°, TITAN 3C TRANSTAGE R/B passes over latitudes between 17.6°N and 17.6°S, concentrating coverage over equatorial and near-equatorial regions. Low-inclination orbits maximise revisit rates over specific tropical zones. 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 3C TRANSTAGE R/B follows a Highly Elliptical Orbit, swinging between 7,720 km (perigee) and 120,890 km (apogee). It spends most of its 51.9 hours orbital period near apogee, moving slowly at high altitude — effectively loitering over a region of interest before rapidly sweeping through perigee.
TITAN 3C TRANSTAGE R/B (NORAD ID 3956) 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 3C TRANSTAGE R/B was launched on 1969-05-23 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. View the full satellite launch log.
Yes — Orbital Radar tracks TITAN 3C TRANSTAGE R/B (NORAD ID 3956) 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 3C TRANSTAGE R/B’s speed varies dramatically throughout its orbit. At perigee it moves at its fastest, and at apogee it slows to a fraction of that — this is Kepler’s second law in action. Its average orbital velocity is approximately 8,549 km/h (2.37 km/s), completing one revolution every 51.9 hours. Learn more about highly elliptical orbits.