DELTA 1 R/B
NORAD 1433
Rocket Body
LEO
1965-051B
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LEO · NORAD 1433
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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
657 km
Apogee
711 km
Inclination
98.6°
Period
98.4 min
Mean Motion
14.62813910 rev/day
TLE Epoch
2026-09-16 04:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude684 km
Orbital Velocity27,060 km/h
Velocity7.52 km/s
Orbital Period98 minutes
Orbits / Day14.63
Eccentricity0.0038
Semi-Major Axis7,055 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~10–25 years
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
1965-07-02
Launch Site
Cape Canaveral Space Force Station, United States
Int'l Designator
1965-051B
Object Type
Rocket Body
RCS Size
Medium (0.1–1 m²)
📖 About This Object
DELTA 1 R/B is a spent rocket body associated with United States, launched on 1965-07-02 from Cape Canaveral Space Force Station, United States on the Tiros OT1 launch. After more than 61 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 657 km and 711 km with an inclination of 98.6°. It travels at approximately 27,060 km/h (7.52 km/s), completing one full orbit every 98 minutes — that’s roughly 14.63 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 684 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 342 active payloads and 1,390 tracked debris or rocket body fragments — notable neighbours include TERRA, AQUA, ONEWEB-0179. With an inclination of 98.6°, DELTA 1 R/B passes over latitudes between 98.6°N and 98.6°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 97 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 684 km altitude. Its 98.6° 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 98 minutes, travelling at 27,060 km/h.
DELTA 1 R/B (NORAD ID 1433) 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 1965-07-02 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. 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 1433) 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 27,060 km/h (16,814 mph) — roughly 7.52 km/s. It completes 14.63 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 29 sunrises and sunsets every 24 hours.