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 26550U 26066.80128264 +.00000000 +00000-0 +63786-4 0 00006
2 26550 64.5619 226.6907 0506618 54.9648 309.7863 13.82061852 07
| Epoch (UTC): | 07 March 2026 19:13:50 |
| Eccentricity: | 0.0506618 |
| inclination: | 64.5619° |
| perigee height: | 585 km |
| apogee height: | 1328 km |
| right ascension of ascending node: | 226.6907° |
| argument of perigee: | 54.9648° |
| revolutions per day: | 13.82061852 |
| mean anomaly at epoch: | 309.7863° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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