ELECTRON SECOND STAGE, 100562
Orbit data source: Space-Track
ELECTRON SECOND STAGE, 100562 is a payload satellite owned by Rocket Lab (JP) in LEO that was launched on Wed, 02 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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100562 intel report (Beta)
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Identifier
Orbit
Country
JP / JPNRelated business
Manufacturer
Rocket Lab
Mission
Spacecraft
Bus & Motor
ELECTRON ST2, Unknown motor
Mass
250 kg wet, ~250 kg dry
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
CYL, 1.2 m
Radar Cross Section
RCS unknown
Expand to show TLE details & historyLast TLE update: 2 days ago
TLE from 2 days ago
0 ELECTRON SECOND STAGE
1 A0562U 26201B 26246.54739542 .00322627 30667-4 77077-3 0 9992
2 A0562 38.0466 64.7422 0267370 294.3041 63.0032 15.55781007 165Epoch: 2026-09-03T13:08Z
TLE epoch observation values (Epoch: 2026-09-03T13:08:14.964Z)
Latitude
-0.00002°
Longitude
-115.00417°
Altitude
320.772 km
Speed
7.762 km/s
True Right ascension
04h 18m 58s
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
19:40:29
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
583.986 km
Perigee altitude
221.388 km
Semi-major axis
6,780.824 km
Eccentricity
0.02674
Inclination
38.0466°
RAAN
64.7422°
Arg. of periapsis
294.3041°
True anomaly
65.77412°
Mean anomaly
63.0032°
Eccentric anomaly
64.38455°
Mean motion
3.88704 °/min
Orbital period
92.62 mins
BSTAR
0.00077077
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Other satellites on launch #201 in the year 2026 (2026-09-02 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.ELECTRON SECOND STAGE 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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-09-05 14:37:52.987Z | 185.651° SSW | 2026-09-05 14:39:52.987Z | 141.981° SSE | 17.73° | 2026-09-05 14:41:52.987Z | 107.905° ESE |
| 5 mins | 2026-09-05 16:14:52.987Z | 229.711° WSW | 2026-09-05 16:16:52.987Z | 139.581° SSE | 37.077° | 2026-09-05 16:19:52.987Z | 92.864° ESE |
| 6 mins | 2026-09-05 17:51:52.987Z | 257.779° W | 2026-09-05 17:53:52.987Z | 173.592° S | 42.13° | 2026-09-05 17:57:52.987Z | 103.243° ESE |
| 6 mins | 2026-09-05 19:28:52.987Z | 252.35° W | 2026-09-05 19:30:52.987Z | 206.297° SW | 30.192° | 2026-09-05 19:34:52.987Z | 134.448° 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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