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 59034U 26145.49089344 +.00000000 +00000-0 +22682-4 0 00007
2 59034 43.0028 309.8619 0001009 276.6883 83.3854 15.27577698 04
| Epoch (UTC): | 25 May 2026 11:46:53 |
| Eccentricity: | 0.0001009 |
| inclination: | 43.0028° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 309.8619° |
| argument of perigee: | 276.6883° |
| revolutions per day: | 15.27577698 |
| mean anomaly at epoch: | 83.3854° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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