ELEKTRON / RB, 100830
Orbit data source: Space-Track
ELEKTRON / RB, 100830 is a Japanese payload satellite in LEO that was launched on Sat, 26 Sep 2026 UTC launched from the Rocket Lab Launch Complex (RLLC). Payload-class satellites include a variety of spacecraft equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.
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100830 intel report (Beta)
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Identifier
Orbit
Country
JP / JPNRelated business
None
Manufacturer
Unknown
Mission
Operational spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Unknown
Radar Cross Section
RCS unknown
Expand to show TLE details & historyLast TLE update: 15 hours ago
TLE from 15 hours ago
0 ELEKTRON / RB
1 A0830U 26223B 26270.31659764 .02161409 38656-5 11549-2 0 9992
2 A0830 37.8808 275.3585 0259317 300.8570 56.6940 15.74895301 218Epoch: 2026-09-27T07:35Z
TLE epoch observation values (Epoch: 2026-09-27T07:35:54.036Z)
Latitude
0.00001°
Longitude
155.2713°
Altitude
251.639 km
Speed
7.811 km/s
True Right ascension
18h 21m 26s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
15:43:16
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
522.198 km
Perigee altitude
173.369 km
Semi-major axis
6,725.92 km
Eccentricity
0.02593
Inclination
37.8808°
RAAN
275.3585°
Arg. of periapsis
300.857°
True anomaly
59.22163°
Mean anomaly
56.694°
Eccentric anomaly
57.95337°
Mean motion
3.93474 °/min
Orbital period
91.49 mins
BSTAR
0.0011549
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Other satellites on launch #223 in the year 2026 (2026-09-26 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.ELEKTRON / RB Visibility forecast
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-09-28 05:09:53.522Z | 226.283° WSW | 2026-09-28 05:11:53.522Z | 143.2° SSE | 42.904° | 2026-09-28 05:14:53.522Z | 93.2° ESE |
| 6 mins | 2026-09-28 06:44:53.522Z | 260.589° W | 2026-09-28 06:47:53.522Z | 141.641° SSE | 55.752° | 2026-09-28 06:50:53.522Z | 102.447° ESE |
| 6 mins | 2026-09-28 08:20:53.522Z | 256.748° W | 2026-09-28 08:22:53.522Z | 213.876° SW | 34.475° | 2026-09-28 08:26:53.522Z | 131.142° SE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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