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 55418U 26145.54181977 +.00000000 +00000-0 -19872-3 0 00007
2 55418 69.9992 250.6898 0003177 268.7510 91.3285 14.98342719 00
| Epoch (UTC): | 25 May 2026 13:00:13 |
| Eccentricity: | 0.0003177 |
| inclination: | 69.9992° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 250.6898° |
| argument of perigee: | 268.7510° |
| revolutions per day: | 14.98342719 |
| mean anomaly at epoch: | 91.3285° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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