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 55293U 26145.42429154 +.00000000 +00000-0 +20734-5 0 00007
2 55293 69.9985 190.9637 0003679 267.8414 92.2324 14.98332047 07
| Epoch (UTC): | 25 May 2026 10:10:58 |
| Eccentricity: | 0.0003679 |
| inclination: | 69.9985° |
| perigee height: | 569 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 190.9637° |
| argument of perigee: | 267.8414° |
| revolutions per day: | 14.98332047 |
| mean anomaly at epoch: | 92.2324° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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