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 54775U 26145.47725227 +.00000000 +00000-0 +10453-3 0 00001
2 54775 53.2129 59.2435 0001119 88.1907 271.9214 15.08829237 06
| Epoch (UTC): | 25 May 2026 11:27:14 |
| Eccentricity: | 0.0001119 |
| inclination: | 53.2129° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 59.2435° |
| argument of perigee: | 88.1907° |
| revolutions per day: | 15.08829237 |
| mean anomaly at epoch: | 271.9214° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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