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 59173U 26145.37786720 +.00000000 +00000-0 +28206-4 0 00008
2 59173 43.0029 33.9661 0001211 272.5088 87.5625 15.27578469 07
| Epoch (UTC): | 25 May 2026 09:04:07 |
| Eccentricity: | 0.0001211 |
| inclination: | 43.0029° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 33.9661° |
| argument of perigee: | 272.5088° |
| revolutions per day: | 15.27578469 |
| mean anomaly at epoch: | 87.5625° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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