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ELEKTRON / RB

NORAD 100830 Payload LEO 2026-223B ● Active
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🛰️ Orbital Parameters
Perigee
172 km
Apogee
538 km
Inclination
37.9°
Period
91.6 min
Mean Motion
15.70174680 rev/day
TLE Epoch
2026-09-26 05:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude355 km
Orbital Velocity27,714 km/h
Velocity7.70 km/s
Orbital Period92 minutes
Orbits / Day15.70
Eccentricity0.0272
Semi-Major Axis6,726 km
Est. Orbital LifetimeMonths to ~1 year
🚀 Launch & Identity
Country / Operator
🇯🇵 Japan
Launch Date
2026-09-26
Launch Site
Rocket Lab Launch Complex 1, New Zealand
Int'l Designator
2026-223B
Object Type
Payload
RCS Size
Unknown
📖 About This Object
ELEKTRON / RB is an active satellite operated by Japan, launched on 2026-09-26 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 172 km and 538 km with an inclination of 37.9°. It travels at approximately 27,714 km/h (7.70 km/s), completing one full orbit every 92 minutes — that’s roughly 15.70 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is months to ~1 year. Orbital Radar tracks ELEKTRON / RB in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
ELEKTRON / RB orbits at an average altitude of 355 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 ELEKTRON / RB’s average altitude, there are currently 1,047 active payloads and 39 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 5.6% of all active satellites. With an inclination of 37.9°, ELEKTRON / RB passes over latitudes between 37.9°N and 37.9°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. Japan operates approximately 208 active satellites in total, of which 5 share a similar altitude band with ELEKTRON / RB.
❓ Frequently Asked Questions
ELEKTRON / RB orbits in Low Earth Orbit (LEO) at altitudes between 172 km (perigee) and 538 km (apogee), with an average altitude of approximately 355 km. It completes one orbit every 92 minutes, travelling at approximately 27,714 km/h (17,220 mph).
ELEKTRON / RB is operated by Japan. It is catalogued by the U.S. Space Surveillance Network under NORAD ID 100830. You can track ELEKTRON / RB in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
ELEKTRON / RB was launched on 2026-09-26 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 ELEKTRON / RB (NORAD ID 100830) 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.
ELEKTRON / RB travels at approximately 27,714 km/h (17,220 mph) — roughly 7.70 km/s. It completes 15.70 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 31 sunrises and sunsets every 24 hours.