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 41793U 26113.08100116 +.00000000 +00000-0 +00000-0 0 00007
2 41793 0.0586 79.9180 0004870 335.1613 259.2275 1.00271565 09
| Epoch (UTC): | 23 April 2026 01:56:38 |
| Eccentricity: | 0.0004870 |
| inclination: | 0.0586° |
| perigee height: | 35766 km |
| apogee height: | 35807 km |
| right ascension of ascending node: | 79.9180° |
| argument of perigee: | 335.1613° |
| revolutions per day: | 1.00271565 |
| mean anomaly at epoch: | 259.2275° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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