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 26536U 26100.15981271 +.00000000 +00000-0 +69516-4 0 00009
2 26536 98.4674 118.0194 0011289 132.5230 227.6899 14.13907298 00
| Epoch (UTC): | 10 April 2026 03:50:07 |
| Eccentricity: | 0.0011289 |
| inclination: | 98.4674° |
| perigee height: | 838 km |
| apogee height: | 854 km |
| right ascension of ascending node: | 118.0194° |
| argument of perigee: | 132.5230° |
| revolutions per day: | 14.13907298 |
| mean anomaly at epoch: | 227.6899° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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