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 59346U 26145.59083514 +.00000000 +00000-0 +00000-0 0 00003
2 59346 0.0172 312.3585 0000243 166.1284 13.2527 1.00270080 01
| Epoch (UTC): | 25 May 2026 14:10:48 |
| Eccentricity: | 0.0000243 |
| inclination: | 0.0172° |
| perigee height: | 35786 km |
| apogee height: | 35788 km |
| right ascension of ascending node: | 312.3585° |
| argument of perigee: | 166.1284° |
| revolutions per day: | 1.00270080 |
| mean anomaly at epoch: | 13.2527° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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