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 59006U 26145.55518442 +.00000000 +00000-0 -36285-5 0 00005
2 59006 53.1604 80.9540 0001140 94.8578 265.2553 15.30188369 06
| Epoch (UTC): | 25 May 2026 13:19:27 |
| Eccentricity: | 0.0001140 |
| inclination: | 53.1604° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 80.9540° |
| argument of perigee: | 94.8578° |
| revolutions per day: | 15.30188369 |
| mean anomaly at epoch: | 265.2553° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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