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 59043U 26145.50245780 +.00000000 +00000-0 +54802-4 0 00006
2 59043 43.0034 309.9487 0000827 280.5034 79.5724 15.27571164 09
| Epoch (UTC): | 25 May 2026 12:03:32 |
| Eccentricity: | 0.0000827 |
| inclination: | 43.0034° |
| perigee height: | 483 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 309.9487° |
| argument of perigee: | 280.5034° |
| revolutions per day: | 15.27571164 |
| mean anomaly at epoch: | 79.5724° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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