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 62828U 26145.46371866 +.00000000 +00000-0 +10643-2 0 00004
2 62828 53.1598 309.3830 0000688 63.7879 296.3194 15.34413505 02
| Epoch (UTC): | 25 May 2026 11:07:45 |
| Eccentricity: | 0.0000688 |
| inclination: | 53.1598° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 309.3830° |
| argument of perigee: | 63.7879° |
| revolutions per day: | 15.34413505 |
| mean anomaly at epoch: | 296.3194° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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