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DELTA 1 R/B(1)

NORAD 10295 Rocket Body MEO 1977-080B
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
871 km
Apogee
2074 km
Inclination
27.1°
Period
115.4 min
Mean Motion
12.48112411 rev/day
TLE Epoch
2026-06-25 17:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude1,473 km
Orbital Velocity25,664 km/h
Velocity7.13 km/s
Orbital Period115 minutes
Orbits / Day12.48
Eccentricity0.0767
Semi-Major Axis7,844 km
Est. Orbital LifetimeThousands of years
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
1977-08-25
Launch Site
Cape Canaveral, Florida
Int'l Designator
1977-080B
Object Type
Rocket Body
RCS Size
Large (>1 m²)
📖 About This Object
DELTA 1 R/B(1) is a spent rocket body associated with United States, launched on 1977-08-25 from Cape Canaveral, Florida on the Sirio 1 launch. With over 49 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Medium Earth Orbit (MEO) at altitudes between 871 km and 2,074 km with an inclination of 27.1°. It travels at approximately 25,664 km/h (7.13 km/s), completing one full orbit every 115 minutes — that’s roughly 12.48 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is thousands of years. Spent rocket bodies like DELTA 1 R/B(1) 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 1 R/B(1) orbits at an average altitude of 1,473 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 DELTA 1 R/B(1)’s average altitude, there are currently 314 active payloads and 249 tracked debris or rocket body fragments. With an inclination of 27.1°, DELTA 1 R/B(1) passes over latitudes between 27.1°N and 27.1°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
DELTA 1 R/B(1) orbits in Medium Earth Orbit (MEO) at altitudes between 871 km (perigee) and 2,074 km (apogee), with an average altitude of approximately 1,473 km. It completes one orbit every 115 minutes, travelling at approximately 25,664 km/h (15,947 mph).
DELTA 1 R/B(1) (NORAD ID 10295) 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 1 R/B(1) was launched on 1977-08-25 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. At its current altitude, the estimated remaining orbital lifetime is: thousands of years. View the full satellite launch log.
Yes — Orbital Radar tracks DELTA 1 R/B(1) (NORAD ID 10295) 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 1 R/B(1) travels at approximately 25,664 km/h (15,947 mph) — roughly 7.13 km/s. It completes 12.48 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 25 sunrises and sunsets every 24 hours.