PEGASUS R/B
NORAD 69793
Rocket Body
LEO
2026-152B
CONNECTING…
LEO · NORAD 69793
NOW PASSING OVER
Calculating position…
—
Altitude (km)
—
Speed (km/s)
—
Latitude
—
Longitude
🛰️ Orbital Parameters
Perigee
331 km
Apogee
357 km
Inclination
20.6°
Period
91.4 min
Mean Motion
15.75210739 rev/day
TLE Epoch
2026-10-08 13:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude344 km
Orbital Velocity27,736 km/h
Velocity7.70 km/s
Orbital Period91 minutes
Orbits / Day15.75
Eccentricity0.0019
Semi-Major Axis6,715 km
Est. Orbital LifetimeMonths to ~1 year
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
2026-07-03
Launch Site
Kwajalein Atoll / Omelek, Marshall Islands
Int'l Designator
2026-152B
Object Type
Rocket Body
RCS Size
Large (>1 m²)
📖 About This Object
PEGASUS R/B is a spent rocket body associated with United States, launched on 2026-07-03 from Kwajalein Atoll / Omelek, Marshall Islands on the Swift Reboost launch. As a relatively recent addition to the catalogue, its orbital elements are well-characterised. It orbits in Low Earth Orbit (LEO) at altitudes between 331 km and 357 km with an inclination of 20.6°. It travels at approximately 27,736 km/h (7.70 km/s), completing one full orbit every 91 minutes — that’s roughly 15.75 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is months to ~1 year. Spent rocket bodies like PEGASUS 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
PEGASUS R/B orbits at an average altitude of 344 km in the lower reaches of Low Earth Orbit, where atmospheric drag is significant and orbital lifetimes are measured in months to a few years. This is the busiest corridor in space — home to crewed spacecraft, rapid-revisit imaging satellites and the densest part of the Starlink constellation. Within ±50 km of PEGASUS R/B’s average altitude, there are currently 1,015 active payloads and 41 tracked debris or rocket body fragments — notable neighbours include STARLINK-1008, STARLINK-1012, STARLINK-1020. This makes it one of the more crowded altitude bands, containing roughly 5.4% of all active satellites. With an inclination of 20.6°, PEGASUS R/B passes over latitudes between 20.6°N and 20.6°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 13,208 active satellites in total, of which 946 share a similar altitude band with PEGASUS 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
PEGASUS R/B orbits in Low Earth Orbit (LEO) at altitudes between 331 km (perigee) and 357 km (apogee), with an average altitude of approximately 344 km. It completes one orbit every 91 minutes, travelling at approximately 27,736 km/h (17,235 mph).
PEGASUS R/B (NORAD ID 69793) 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.
PEGASUS R/B was launched on 2026-07-03 from Kwajalein Atoll / Omelek, Marshall Islands. At its current altitude, the estimated remaining orbital lifetime is: months to ~1 year. View the full satellite launch log.
Yes — Orbital Radar tracks PEGASUS R/B (NORAD ID 69793) 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.
PEGASUS R/B travels at approximately 27,736 km/h (17,235 mph) — roughly 7.70 km/s. It completes 15.75 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 32 sunrises and sunsets every 24 hours.