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 59385U 26145.46490359 +.00000000 +00000-0 +64567-2 0 00001
2 59385 53.1601 259.2177 0004703 118.6745 241.4729 15.31829489 06
| Epoch (UTC): | 25 May 2026 11:09:27 |
| Eccentricity: | 0.0004703 |
| inclination: | 53.1601° |
| perigee height: | 467 km |
| apogee height: | 474 km |
| right ascension of ascending node: | 259.2177° |
| argument of perigee: | 118.6745° |
| revolutions per day: | 15.31829489 |
| mean anomaly at epoch: | 241.4729° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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