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 59495U 26145.39377177 +.00000000 +00000-0 +26690-4 0 00004
2 59495 43.0036 266.8105 0001554 278.7449 81.3227 15.27578167 06
| Epoch (UTC): | 25 May 2026 09:27:01 |
| Eccentricity: | 0.0001554 |
| inclination: | 43.0036° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 266.8105° |
| argument of perigee: | 278.7449° |
| revolutions per day: | 15.27578167 |
| mean anomaly at epoch: | 81.3227° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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