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 59268U 26145.36698745 +.00000000 +00000-0 +79144-3 0 00007
2 59268 53.1596 185.1535 0002057 84.2870 275.8365 15.30217695 07
| Epoch (UTC): | 25 May 2026 08:48:27 |
| Eccentricity: | 0.0002057 |
| inclination: | 53.1596° |
| perigee height: | 474 km |
| apogee height: | 477 km |
| right ascension of ascending node: | 185.1535° |
| argument of perigee: | 84.2870° |
| revolutions per day: | 15.30217695 |
| mean anomaly at epoch: | 275.8365° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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