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DELTA 1 R/B

NORAD 6127 Rocket Body LEO 1972-058B
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Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
547 km
Apogee
664 km
Inclination
98.5°
Period
96.8 min
Mean Motion
14.87638271 rev/day
TLE Epoch
2026-09-16 04:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude606 km
Orbital Velocity27,212 km/h
Velocity7.56 km/s
Orbital Period97 minutes
Orbits / Day14.88
Eccentricity0.0084
Semi-Major Axis6,977 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~10–25 years
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
1972-07-23
Launch Site
Vandenberg Space Force Base, United States
Int'l Designator
1972-058B
Object Type
Rocket Body
RCS Size
Large (>1 m²)
📖 About This Object
DELTA 1 R/B is a spent rocket body associated with United States, launched on 1972-07-23 from Vandenberg Space Force Base, United States on the ERTS A launch. After more than 54 years in orbit, it is one of the longest-surviving objects in the space catalogue. It orbits in Low Earth Orbit (LEO) at altitudes between 547 km and 664 km with an inclination of 98.5°. It travels at approximately 27,212 km/h (7.56 km/s), completing one full orbit every 97 minutes — that’s roughly 14.88 orbits per day. Its near-polar, sun-synchronous orbit means it passes over any given point on Earth at approximately the same local solar time, ideal for consistent Earth observation lighting conditions. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~10–25 years. Spent rocket bodies like DELTA 1 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 1 R/B orbits at an average altitude of 606 km in a sun-synchronous orbit (SSO), a specialised subset of LEO where the orbital plane precesses to maintain a constant angle relative to the Sun. This provides consistent lighting conditions on every pass — essential for Earth observation, weather monitoring and environmental science. Within ±50 km of DELTA 1 R/B’s average altitude, there are currently 1,639 active payloads and 734 tracked debris or rocket body fragments — notable neighbours include ONEWEB-0050, STARLINK-3005, STARLINK-3090. This makes it one of the more crowded altitude bands, containing roughly 8.8% of all active satellites. With an inclination of 98.5°, DELTA 1 R/B passes over latitudes between 98.5°N and 98.5°S, providing near-global coverage including the polar regions. Polar and near-polar orbits are used for reconnaissance, weather monitoring and Earth-observation missions that need to image every part of the planet. United States operates approximately 13,206 active satellites in total, of which 1,050 share a similar altitude band with DELTA 1 R/B.
🔗 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 is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 606 km altitude. Its 98.5° inclination causes the orbital plane to precess at exactly the rate of the Earth’s revolution around the Sun, so the satellite crosses each latitude at a consistent local solar time. It completes one orbit every 97 minutes, travelling at 27,212 km/h.
DELTA 1 R/B (NORAD ID 6127) 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 was launched on 1972-07-23 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: ~10–25 years. View the full satellite launch log.
Yes — Orbital Radar tracks DELTA 1 R/B (NORAD ID 6127) 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 travels at approximately 27,212 km/h (16,908 mph) — roughly 7.56 km/s. It completes 14.88 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 30 sunrises and sunsets every 24 hours.