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ELECTRON R/B

NORAD 100245 Rocket Body LEO 2026-180C
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Altitude (km)
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Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
206 km
Apogee
320 km
Inclination
42.0°
Period
89.8 min
Mean Motion
16.06457083 rev/day
TLE Epoch
2026-09-21 19:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude263 km
Orbital Velocity27,905 km/h
Velocity7.75 km/s
Orbital Period90 minutes
Orbits / Day16.06
Eccentricity0.0086
Semi-Major Axis6,634 km
Est. Orbital LifetimeWeeks to months
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
2026-08-06
Launch Site
Rocket Lab Launch Complex 1, New Zealand
Int'l Designator
2026-180C
Object Type
Rocket Body
RCS Size
Large (>1 m²)
📖 About This Object
ELECTRON R/B is a spent rocket body associated with United States, launched on 2026-08-06 from Rocket Lab Launch Complex 1, New Zealand on the QPS-SAR-13 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 206 km and 320 km with an inclination of 42.0°. It travels at approximately 27,905 km/h (7.75 km/s), completing one full orbit every 90 minutes — that’s roughly 16.06 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is weeks to months. Spent rocket bodies like ELECTRON 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
ELECTRON R/B orbits at an average altitude of 263 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 ELECTRON R/B’s average altitude, there are currently 90 active payloads and 13 tracked debris or rocket body fragments — notable neighbours include STARLINK-1036, STARLINK-1068, STARLINK-1171. With an inclination of 42.0°, ELECTRON R/B passes over latitudes between 42.0°N and 42.0°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 13,197 active satellites in total, of which 63 share a similar altitude band with ELECTRON 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
ELECTRON R/B orbits in Low Earth Orbit (LEO) at altitudes between 206 km (perigee) and 320 km (apogee), with an average altitude of approximately 263 km. It completes one orbit every 90 minutes, travelling at approximately 27,905 km/h (17,339 mph).
ELECTRON R/B (NORAD ID 100245) 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.
ELECTRON R/B was launched on 2026-08-06 from Rocket Lab Launch Complex 1, New Zealand. At its current altitude, the estimated remaining orbital lifetime is: weeks to months. View the full satellite launch log.
Yes — Orbital Radar tracks ELECTRON R/B (NORAD ID 100245) 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.
ELECTRON R/B travels at approximately 27,905 km/h (17,339 mph) — roughly 7.75 km/s. It completes 16.06 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 32 sunrises and sunsets every 24 hours.