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ELECTRON SECOND STAGE

NORAD 100562 Payload LEO 2026-201B ● Active
CONNECTING… LEO · NORAD 100562
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
219 km
Apogee
581 km
Inclination
38.0°
Period
92.6 min
Mean Motion
15.55781007 rev/day
TLE Epoch
2026-09-03 13:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude400 km
Orbital Velocity27,621 km/h
Velocity7.67 km/s
Orbital Period93 minutes
Orbits / Day15.56
Eccentricity0.0267
Semi-Major Axis6,771 km
Est. Orbital Lifetime~1–3 years
🚀 Launch & Identity
Country / Operator
🇯🇵 Japan
Launch Date
2026-09-02
Launch Site
RLLC
Int'l Designator
2026-201B
Object Type
Payload
RCS Size
Unknown
📖 About This Object
ELECTRON SECOND STAGE is an active satellite operated by Japan, launched on 2026-09-02 from RLLC. As a relatively recent addition to the catalogue, its orbital elements are well-characterised. It orbits in Low Earth Orbit (LEO) at altitudes between 219 km and 581 km with an inclination of 38.0°. It travels at approximately 27,621 km/h (7.67 km/s), completing one full orbit every 93 minutes — that’s roughly 15.56 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~1–3 years. Orbital Radar tracks ELECTRON SECOND STAGE in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
ELECTRON SECOND STAGE orbits at an average altitude of 400 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 SECOND STAGE’s average altitude, there are currently 1,145 active payloads and 86 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 6.3% of all active satellites. With an inclination of 38.0°, ELECTRON SECOND STAGE passes over latitudes between 38.0°N and 38.0°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. Japan operates approximately 205 active satellites in total, of which 6 share a similar altitude band with ELECTRON SECOND STAGE.
❓ Frequently Asked Questions
ELECTRON SECOND STAGE orbits in Low Earth Orbit (LEO) at altitudes between 219 km (perigee) and 581 km (apogee), with an average altitude of approximately 400 km. It completes one orbit every 93 minutes, travelling at approximately 27,621 km/h (17,163 mph).
ELECTRON SECOND STAGE is operated by Japan. It is catalogued by the U.S. Space Surveillance Network under NORAD ID 100562. You can track ELECTRON SECOND STAGE in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
ELECTRON SECOND STAGE was launched on 2026-09-02 from RLLC. At its current altitude, the estimated remaining orbital lifetime is: ~1–3 years. View the full satellite launch log.
Yes — Orbital Radar tracks ELECTRON SECOND STAGE (NORAD ID 100562) 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 SECOND STAGE travels at approximately 27,621 km/h (17,163 mph) — roughly 7.67 km/s. It completes 15.56 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 31 sunrises and sunsets every 24 hours.