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 59249U 26145.51826036 +.00000000 +00000-0 -43657-4 0 00001
2 59249 43.0049 69.8419 0001370 264.4728 95.5967 15.27587042 04
| Epoch (UTC): | 25 May 2026 12:26:17 |
| Eccentricity: | 0.0001370 |
| inclination: | 43.0049° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 69.8419° |
| argument of perigee: | 264.4728° |
| revolutions per day: | 15.27587042 |
| mean anomaly at epoch: | 95.5967° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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