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 55268U 26142.53471350 +.00000000 +00000-0 +00000-0 0 00002
2 55268 55.1207 149.5238 0008482 318.2622 45.1799 2.00573116 06
| Epoch (UTC): | 22 May 2026 12:49:59 |
| Eccentricity: | 0.0008482 |
| inclination: | 55.1207° |
| perigee height: | 20159 km |
| apogee height: | 20204 km |
| right ascension of ascending node: | 149.5238° |
| argument of perigee: | 318.2622° |
| revolutions per day: | 2.00573116 |
| mean anomaly at epoch: | 45.1799° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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