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 59442U 26145.65685071 +.00000000 +00000-0 +34617-3 0 00007
2 59442 45.6163 243.6311 0012052 333.2372 26.7901 15.35159522 07
| Epoch (UTC): | 25 May 2026 15:45:51 |
| Eccentricity: | 0.0012052 |
| inclination: | 45.6163° |
| perigee height: | 452 km |
| apogee height: | 469 km |
| right ascension of ascending node: | 243.6311° |
| argument of perigee: | 333.2372° |
| revolutions per day: | 15.35159522 |
| mean anomaly at epoch: | 26.7901° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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