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 59197U 26145.35537453 +.00000000 +00000-0 +56484-3 0 00007
2 59197 43.0049 19.8114 0000924 270.5700 89.5046 15.27585798 02
| Epoch (UTC): | 25 May 2026 08:31:44 |
| Eccentricity: | 0.0000924 |
| inclination: | 43.0049° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 19.8114° |
| argument of perigee: | 270.5700° |
| revolutions per day: | 15.27585798 |
| mean anomaly at epoch: | 89.5046° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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