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 55110U 26145.51774600 +.00000000 +00000-0 +40630-3 0 00009
2 55110 97.5551 238.2455 0006417 287.3356 72.7181 15.27438902 04
| Epoch (UTC): | 25 May 2026 12:25:33 |
| Eccentricity: | 0.0006417 |
| inclination: | 97.5551° |
| perigee height: | 479 km |
| apogee height: | 488 km |
| right ascension of ascending node: | 238.2455° |
| argument of perigee: | 287.3356° |
| revolutions per day: | 15.27438902 |
| mean anomaly at epoch: | 72.7181° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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