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 62564U 26145.39039845 +.00000000 +00000-0 +14507-2 0 00004
2 62564 42.9982 37.7261 0002883 277.9641 82.0899 15.70914260 03
| Epoch (UTC): | 25 May 2026 09:22:10 |
| Eccentricity: | 0.0002883 |
| inclination: | 42.9982° |
| perigee height: | 354 km |
| apogee height: | 358 km |
| right ascension of ascending node: | 37.7261° |
| argument of perigee: | 277.9641° |
| revolutions per day: | 15.70914260 |
| mean anomaly at epoch: | 82.0899° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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