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 59542U 26145.04069160 +.00000000 +00000-0 +39925-4 0 00004
2 59542 42.9987 272.1280 0001290 260.4177 99.6529 15.27578108 01
| Epoch (UTC): | 25 May 2026 00:58:35 |
| Eccentricity: | 0.0001290 |
| inclination: | 42.9987° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 272.1280° |
| argument of perigee: | 260.4177° |
| revolutions per day: | 15.27578108 |
| mean anomaly at epoch: | 99.6529° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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