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 59005U 26145.54779647 +.00000000 +00000-0 +23027-4 0 00007
2 59005 53.1611 80.9109 0001343 91.1049 269.0106 15.30192610 02
| Epoch (UTC): | 25 May 2026 13:08:49 |
| Eccentricity: | 0.0001343 |
| inclination: | 53.1611° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 80.9109° |
| argument of perigee: | 91.1049° |
| revolutions per day: | 15.30192610 |
| mean anomaly at epoch: | 269.0106° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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