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 55309U 26145.38232395 +.00000000 +00000-0 -21879-3 0 00009
2 55309 69.9987 170.9448 0003698 268.9893 91.0842 14.98342591 06
| Epoch (UTC): | 25 May 2026 09:10:32 |
| Eccentricity: | 0.0003698 |
| inclination: | 69.9987° |
| perigee height: | 569 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 170.9448° |
| argument of perigee: | 268.9893° |
| revolutions per day: | 14.98342591 |
| mean anomaly at epoch: | 91.0842° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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