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 41786U 26145.62532941 +.00000000 +00000-0 +17353-3 0 00001
2 41786 97.9904 208.3304 0000816 71.3902 288.7393 14.70838775 03
| Epoch (UTC): | 25 May 2026 15:00:28 |
| Eccentricity: | 0.0000816 |
| inclination: | 97.9904° |
| perigee height: | 658 km |
| apogee height: | 659 km |
| right ascension of ascending node: | 208.3304° |
| argument of perigee: | 71.3902° |
| revolutions per day: | 14.70838775 |
| mean anomaly at epoch: | 288.7393° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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