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PEGASUS R/B

NORAD 41892 Rocket Body LEO 2016-078J
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
330 km
Apogee
340 km
Inclination
34.9°
Period
91.2 min
Mean Motion
15.78705150 rev/day
TLE Epoch
2026-06-25 21:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude335 km
Orbital Velocity27,755 km/h
Velocity7.71 km/s
Orbital Period91 minutes
Orbits / Day15.79
Eccentricity0.0007
Semi-Major Axis6,706 km
Est. Orbital LifetimeMonths to ~1 year
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
2016-12-15
Launch Site
Esrange, Sweden
Int'l Designator
2016-078J
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 2016-12-15 from Esrange, Sweden on the CYGNSS launch. After 10 years in orbit, it continues to be tracked by global surveillance networks. It orbits in Low Earth Orbit (LEO) at altitudes between 330 km and 340 km with an inclination of 34.9°. It travels at approximately 27,755 km/h (7.71 km/s), completing one full orbit every 91 minutes — that’s roughly 15.79 orbits per day. Its near-circular orbit (eccentricity close to zero) means it maintains a very consistent altitude throughout each revolution. 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 335 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 1,119 active payloads and 35 tracked debris or rocket body fragments — notable neighbours include STARLINK-1036, STARLINK-1043, STARLINK-1048. This makes it one of the more crowded altitude bands, containing roughly 6.4% of all active satellites. With an inclination of 34.9°, PEGASUS R/B passes over latitudes between 34.9°N and 34.9°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 1,054 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 330 km (perigee) and 340 km (apogee), with an average altitude of approximately 335 km. It completes one orbit every 91 minutes, travelling at approximately 27,755 km/h (17,246 mph).
PEGASUS R/B (NORAD ID 41892) 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 2016-12-15 from Esrange, Sweden. 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 41892) 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 27,755 km/h (17,246 mph) — roughly 7.71 km/s. It completes 15.79 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 32 sunrises and sunsets every 24 hours.