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DELTA 4 R/B

NORAD 32288 Rocket Body GEO 2007-054B
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
36010 km
Apogee
38125 km
Inclination
11.5°
Period
1502.0 min
Mean Motion
0.95871103 rev/day
TLE Epoch
2026-06-26 01:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude37,068 km
Orbital Velocity10,905 km/h
Velocity3.03 km/s
Orbital Period25.0 hours
Orbits / Day0.96
Eccentricity0.0243
Semi-Major Axis43,439 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
2007-11-11
Launch Site
Cape Canaveral, Florida
Int'l Designator
2007-054B
Object Type
Rocket Body
RCS Size
Medium (0.1–1 m²)
📖 About This Object
DELTA 4 R/B is a spent rocket body associated with United States, launched on 2007-11-11 from Cape Canaveral, Florida on the DSP F23 launch. After 19 years in orbit, it continues to be tracked by global surveillance networks. It orbits in Geostationary Orbit (GEO) at altitudes between 36,010 km and 38,125 km with an inclination of 11.5°. It travels at approximately 10,905 km/h (3.03 km/s), completing one full orbit every 25.0 hours — that’s roughly 0.96 orbits per day. At geostationary altitude, there is no meaningful atmospheric drag — this object will remain in orbit indefinitely unless actively deorbited. Spent rocket bodies like DELTA 4 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
DELTA 4 R/B occupies geostationary orbit at approximately 35,786 km above the equator, where its orbital period matches the Earth’s 24-hour rotation. From the ground, it appears to hover over a fixed point — ideal for broadcast television, weather monitoring and wideband communications. With an inclination of 11.5°, it traces a small figure-of-eight pattern relative to the equator rather than remaining perfectly stationary, which can indicate aging stationkeeping fuel or a deliberate inclined-orbit strategy. Within ±50 km of DELTA 4 R/B’s average altitude, there are currently 4 active payloads and 1 tracked debris or rocket body fragment. 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
DELTA 4 R/B orbits at approximately 37,068 km altitude, where the orbital period matches the Earth’s 24-hour rotation. This means it stays above the same point on the equator at all times. Its actual speed is still 10,905 km/h — it just keeps pace with the ground below. With an inclination of 11.5°, it actually traces a small figure-of-eight pattern rather than remaining perfectly fixed. Learn more about geostationary orbits.
DELTA 4 R/B (NORAD ID 32288) 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.
DELTA 4 R/B was launched on 2007-11-11 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 DELTA 4 R/B (NORAD ID 32288) 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.
DELTA 4 R/B travels at approximately 10,905 km/h (6,776 mph) — roughly 3.03 km/s. Despite this high speed, it appears stationary from the ground because it matches the Earth’s rotation. Geostationary satellites are actually slower than LEO satellites because orbital velocity decreases with altitude.