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 59259U 26145.46806977 +.00000000 +00000-0 +21176-4 0 00009
2 59259 53.1596 184.3714 0001042 83.3018 276.8102 15.30196013 04
| Epoch (UTC): | 25 May 2026 11:14:01 |
| Eccentricity: | 0.0001042 |
| inclination: | 53.1596° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 184.3714° |
| argument of perigee: | 83.3018° |
| revolutions per day: | 15.30196013 |
| mean anomaly at epoch: | 276.8102° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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