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PEGASUS R/B

NORAD 44629 Rocket Body LEO 2019-068B
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Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
543 km
Apogee
559 km
Inclination
27.0°
Period
95.7 min
Mean Motion
15.05252899 rev/day
TLE Epoch
2026-06-25 13:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude551 km
Orbital Velocity27,318 km/h
Velocity7.59 km/s
Orbital Period96 minutes
Orbits / Day15.05
Eccentricity0.0012
Semi-Major Axis6,922 km
Est. Orbital Lifetime~3–10 years
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
2019-10-11
Launch Site
Esrange, Sweden
Int'l Designator
2019-068B
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 2019-10-11 from Esrange, Sweden on the ICON launch. It orbits in Low Earth Orbit (LEO) at altitudes between 543 km and 559 km with an inclination of 27.0°. It travels at approximately 27,318 km/h (7.59 km/s), completing one full orbit every 96 minutes — that’s roughly 15.05 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~3–10 years. 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 551 km in the core of Low Earth Orbit, the most heavily utilised altitude band. The balance of moderate drag (limiting debris accumulation) and short signal path (enabling low-latency links and high-resolution imaging) makes this regime the default for most commercial and government missions. Within ±50 km of PEGASUS R/B’s average altitude, there are currently 3,330 active payloads and 368 tracked debris or rocket body fragments — notable neighbours include STARLINK-1184, STARLINK-1276, ONEWEB-0050. This makes it one of the more crowded altitude bands, containing roughly 19% of all active satellites. With an inclination of 27.0°, PEGASUS R/B passes over latitudes between 27.0°N and 27.0°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, of which 2,694 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 543 km (perigee) and 559 km (apogee), with an average altitude of approximately 551 km. It completes one orbit every 96 minutes, travelling at approximately 27,318 km/h (16,975 mph).
PEGASUS R/B (NORAD ID 44629) 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 2019-10-11 from Esrange, Sweden. At its current altitude, the estimated remaining orbital lifetime is: ~3–10 years. View the full satellite launch log.
Yes — Orbital Radar tracks PEGASUS R/B (NORAD ID 44629) 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 27,318 km/h (16,975 mph) — roughly 7.59 km/s. It completes 15.05 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 30 sunrises and sunsets every 24 hours.