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 55297U 26145.54946330 +.00000000 +00000-0 +15849-4 0 00004
2 55297 69.9987 190.5974 0003727 267.8407 92.2326 14.98330377 05
| Epoch (UTC): | 25 May 2026 13:11:13 |
| Eccentricity: | 0.0003727 |
| inclination: | 69.9987° |
| perigee height: | 569 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 190.5974° |
| argument of perigee: | 267.8407° |
| revolutions per day: | 14.98330377 |
| mean anomaly at epoch: | 92.2326° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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