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ELECTRON R/B

NORAD 100402 Rocket Body LEO 2026-191B
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🛰️ Orbital Parameters
Perigee
250 km
Apogee
507 km
Inclination
42.0°
Period
92.1 min
Mean Motion
15.63180645 rev/day
TLE Epoch
2026-10-03 02:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude379 km
Orbital Velocity27,665 km/h
Velocity7.68 km/s
Orbital Period92 minutes
Orbits / Day15.63
Eccentricity0.0190
Semi-Major Axis6,750 km
Est. Orbital LifetimeMonths to ~1 year
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
2026-08-20
Launch Site
Rocket Lab Launch Complex 1, New Zealand
Int'l Designator
2026-191B
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 2026-08-20 from Rocket Lab Launch Complex 1, New Zealand on the QPS-SAR-18 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 250 km and 507 km with an inclination of 42.0°. It travels at approximately 27,665 km/h (7.68 km/s), completing one full orbit every 92 minutes — that’s roughly 15.63 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is months to ~1 year. 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 379 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 1,154 active payloads and 65 tracked debris or rocket body fragments — notable neighbours include ISS (ZARYA), STARLINK-1008, STARLINK-1012. This makes it one of the more crowded altitude bands, containing roughly 6.2% of all active satellites. 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 13,225 active satellites in total, of which 1,031 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 250 km (perigee) and 507 km (apogee), with an average altitude of approximately 379 km. It completes one orbit every 92 minutes, travelling at approximately 27,665 km/h (17,190 mph).
ELECTRON R/B (NORAD ID 100402) 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 2026-08-20 from Rocket Lab Launch Complex 1, New Zealand. At its current altitude, the estimated remaining orbital lifetime is: months to ~1 year. View the full satellite launch log.
Yes — Orbital Radar tracks ELECTRON R/B (NORAD ID 100402) 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 27,665 km/h (17,190 mph) — roughly 7.68 km/s. It completes 15.63 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 31 sunrises and sunsets every 24 hours.