ELECTRON R/B
NORAD 101258
Rocket Body
LEO
2026-247B
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LEO · NORAD 101258
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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
235 km
Apogee
588 km
Inclination
42.0°
Period
92.8 min
Mean Motion
15.52383788 rev/day
TLE Epoch
2026-11-03 22:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude412 km
Orbital Velocity27,598 km/h
Velocity7.67 km/s
Orbital Period93 minutes
Orbits / Day15.52
Eccentricity0.0260
Semi-Major Axis6,783 km
Est. Orbital Lifetime~1–3 years
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
2026-11-02
Launch Site
Rocket Lab Launch Complex 1, New Zealand
Int'l Designator
2026-247B
Object Type
Rocket Body
RCS Size
Unknown
📖 About This Object
ELECTRON R/B is a spent rocket body associated with United States, launched on 2026-11-02 from Rocket Lab Launch Complex 1, New Zealand. As a relatively recent addition to the catalogue, its orbital elements are well-characterised. It orbits in Low Earth Orbit (LEO) at altitudes between 235 km and 588 km with an inclination of 42.0°. It travels at approximately 27,598 km/h (7.67 km/s), completing one full orbit every 93 minutes — that’s roughly 15.52 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~1–3 years. 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 412 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 ELECTRON R/B’s average altitude, there are currently 1,345 active payloads and 100 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 6.9% 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 13,350 active satellites in total, of which 1,035 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 235 km (perigee) and 588 km (apogee), with an average altitude of approximately 412 km. It completes one orbit every 93 minutes, travelling at approximately 27,598 km/h (17,149 mph).
ELECTRON R/B (NORAD ID 101258) 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 2026-11-02 from Rocket Lab Launch Complex 1, New Zealand. At its current altitude, the estimated remaining orbital lifetime is: ~1–3 years. View the full satellite launch log.
Yes — Orbital Radar tracks ELECTRON R/B (NORAD ID 101258) 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.
ELECTRON R/B travels at approximately 27,598 km/h (17,149 mph) — roughly 7.67 km/s. It completes 15.52 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 31 sunrises and sunsets every 24 hours.