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 55653U 26145.51792763 +.00000000 +00000-0 -62077-3 0 00001
2 55653 69.9997 350.5790 0002439 268.6114 91.4766 14.98354881 04
| Epoch (UTC): | 25 May 2026 12:25:48 |
| Eccentricity: | 0.0002439 |
| inclination: | 69.9997° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 350.5790° |
| argument of perigee: | 268.6114° |
| revolutions per day: | 14.98354881 |
| mean anomaly at epoch: | 91.4766° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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