View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 26063U 26155.02659226 +.00000000 +00000-0 +77691-4 0 00005
2 26063 100.1911 89.4223 0036524 72.5676 287.9493 14.37959338 07
| Epoch (UTC): | 04 June 2026 00:38:17 |
| Eccentricity: | 0.0036524 |
| inclination: | 100.1911° |
| perigee height: | 739 km |
| apogee height: | 791 km |
| right ascension of ascending node: | 89.4223° |
| argument of perigee: | 72.5676° |
| revolutions per day: | 14.37959338 |
| mean anomaly at epoch: | 287.9493° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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