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 55299U 26145.40341943 +.00000000 +00000-0 +47706-4 0 00007
2 55299 69.9989 190.8913 0003659 267.8773 92.1967 14.98331424 09
| Epoch (UTC): | 25 May 2026 09:40:55 |
| Eccentricity: | 0.0003659 |
| inclination: | 69.9989° |
| perigee height: | 570 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 190.8913° |
| argument of perigee: | 267.8773° |
| revolutions per day: | 14.98331424 |
| mean anomaly at epoch: | 92.1967° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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