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 59725U 26145.43476779 +.00000000 +00000-0 +34183-4 0 00009
2 59725 53.1599 143.3339 0001198 89.3829 270.7310 15.31700215 01
| Epoch (UTC): | 25 May 2026 10:26:03 |
| Eccentricity: | 0.0001198 |
| inclination: | 53.1599° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 143.3339° |
| argument of perigee: | 89.3829° |
| revolutions per day: | 15.31700215 |
| mean anomaly at epoch: | 270.7310° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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