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 59117U 26145.49056921 +.00000000 +00000-0 +24576-3 0 00007
2 59117 97.5610 285.8803 0009132 321.8710 38.1887 15.36172274 07
| Epoch (UTC): | 25 May 2026 11:46:25 |
| Eccentricity: | 0.0009132 |
| inclination: | 97.5610° |
| perigee height: | 451 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 285.8803° |
| argument of perigee: | 321.8710° |
| revolutions per day: | 15.36172274 |
| mean anomaly at epoch: | 38.1887° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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