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 55111U 26145.51916147 +.00000000 +00000-0 +75804-3 0 00005
2 55111 97.5610 239.2558 0005714 67.2212 292.9631 15.30431507 05
| Epoch (UTC): | 25 May 2026 12:27:35 |
| Eccentricity: | 0.0005714 |
| inclination: | 97.5610° |
| perigee height: | 471 km |
| apogee height: | 478 km |
| right ascension of ascending node: | 239.2558° |
| argument of perigee: | 67.2212° |
| revolutions per day: | 15.30431507 |
| mean anomaly at epoch: | 292.9631° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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