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 55145U 26145.46330975 +.00000000 +00000-0 +78849-4 0 00008
2 55145 87.9160 339.9827 0001557 84.1411 275.9899 13.18685372 04
| Epoch (UTC): | 25 May 2026 11:07:09 |
| Eccentricity: | 0.0001557 |
| inclination: | 87.9160° |
| perigee height: | 1189 km |
| apogee height: | 1191 km |
| right ascension of ascending node: | 339.9827° |
| argument of perigee: | 84.1411° |
| revolutions per day: | 13.18685372 |
| mean anomaly at epoch: | 275.9899° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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