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 59029U 26145.47369391 +.00000000 +00000-0 +90219-4 0 00003
2 59029 43.0018 313.1818 0001280 272.0171 88.0534 15.27587260 00
| Epoch (UTC): | 25 May 2026 11:22:07 |
| Eccentricity: | 0.0001280 |
| inclination: | 43.0018° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 313.1818° |
| argument of perigee: | 272.0171° |
| revolutions per day: | 15.27587260 |
| mean anomaly at epoch: | 88.0534° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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