TITAN 3C TRANSTAGE R/B
NORAD 50000
Rocket Body
HEO
1970-027C
CONNECTING…
HEO · NORAD 50000
NOW PASSING OVER
Calculating position…
—
Altitude (km)
—
Speed (km/s)
—
Latitude
—
Longitude
🛰️ Orbital Parameters
Perigee
16000 km
Apogee
116654 km
Inclination
45.5°
Period
3251.7 min
Mean Motion
0.44284934 rev/day
TLE Epoch
2026-06-20 12:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude66,327 km
Orbital Velocity8,430 km/h
Velocity2.34 km/s
Orbital Period54.2 hours
Orbits / Day0.44
Eccentricity0.6923
Semi-Major Axis72,698 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
1970-04-08
Launch Site
Cape Canaveral, Florida
Int'l Designator
1970-027C
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 1970-04-08 from Cape Canaveral, Florida on the Vela 6A launch. After more than 56 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 16,000 km and 116,654 km with an inclination of 45.5°. It travels at approximately 8,430 km/h (2.34 km/s), completing one full orbit every 54.2 hours — that’s roughly 0.44 orbits per day. Its orbital eccentricity of 0.6923 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 16,000 km (perigee) and 116,654 km (apogee). It spends most of its 54.2 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 45.5°, TITAN 3C TRANSTAGE R/B passes over latitudes between 45.5°N and 45.5°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 12,413 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 16,000 km (perigee) and 116,654 km (apogee). It spends most of its 54.2 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 50000) 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 1970-04-08 from Cape Canaveral, Florida, 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 50000) 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 8,430 km/h (2.34 km/s), completing one revolution every 54.2 hours. Learn more about highly elliptical orbits.