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 59866U 26145.56147856 +.00000000 +00000-0 +42437-4 0 00001
2 59866 43.0018 186.1209 0001130 277.2491 82.8232 15.27579044 05
| Epoch (UTC): | 25 May 2026 13:28:31 |
| Eccentricity: | 0.0001130 |
| inclination: | 43.0018° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 186.1209° |
| argument of perigee: | 277.2491° |
| revolutions per day: | 15.27579044 |
| mean anomaly at epoch: | 82.8232° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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