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 59041U 26145.50888563 +.00000000 +00000-0 +11270-3 0 00007
2 59041 43.0014 309.9993 0001516 269.5671 90.5007 15.27570865 01
| Epoch (UTC): | 25 May 2026 12:12:47 |
| Eccentricity: | 0.0001516 |
| inclination: | 43.0014° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 309.9993° |
| argument of perigee: | 269.5671° |
| revolutions per day: | 15.27570865 |
| mean anomaly at epoch: | 90.5007° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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