FIREFLY ALPHA R/B
NORAD 68128
Rocket Body
LEO
2026-046B
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LEO · NORAD 68128
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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
331 km
Apogee
349 km
Inclination
123.1°
Period
91.3 min
Mean Motion
15.76685973 rev/day
TLE Epoch
2026-10-14 17:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude340 km
Orbital Velocity27,745 km/h
Velocity7.71 km/s
Orbital Period91 minutes
Orbits / Day15.77
Eccentricity0.0013
Semi-Major Axis6,711 km
Est. Orbital LifetimeMonths to ~1 year
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
2026-03-12
Launch Site
Vandenberg Space Force Base, United States
Int'l Designator
2026-046B
Object Type
Rocket Body
RCS Size
Large (>1 m²)
📖 About This Object
FIREFLY ALPHA R/B is a spent rocket body associated with United States, launched on 2026-03-12 from Vandenberg Space Force Base, United States on the LM-400 Tech Demo 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 349 km with an inclination of 123.1°. It travels at approximately 27,745 km/h (7.71 km/s), completing one full orbit every 91 minutes — that’s roughly 15.77 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is months to ~1 year. Spent rocket bodies like FIREFLY ALPHA 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
FIREFLY ALPHA R/B orbits at an average altitude of 340 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 FIREFLY ALPHA R/B’s average altitude, there are currently 1,002 active payloads and 38 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 123.1°, FIREFLY ALPHA R/B passes over latitudes between 123.1°N and 123.1°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 13,201 active satellites in total, of which 939 share a similar altitude band with FIREFLY ALPHA 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
FIREFLY ALPHA R/B orbits in Low Earth Orbit (LEO) at altitudes between 331 km (perigee) and 349 km (apogee), with an average altitude of approximately 340 km. It completes one orbit every 91 minutes, travelling at approximately 27,745 km/h (17,240 mph).
FIREFLY ALPHA R/B (NORAD ID 68128) 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.
FIREFLY ALPHA R/B was launched on 2026-03-12 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: months to ~1 year. View the full satellite launch log.
Yes — Orbital Radar tracks FIREFLY ALPHA R/B (NORAD ID 68128) using the latest TLE (two-line element set) orbital data in its live tracking catalogue (see our data sources). 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.
FIREFLY ALPHA R/B travels at approximately 27,745 km/h (17,240 mph) — roughly 7.71 km/s. It completes 15.77 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 32 sunrises and sunsets every 24 hours.