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 55401U 26145.50820414 +.00000000 +00000-0 -28537-4 0 00000
2 55401 69.9993 230.7030 0003550 268.9645 91.1107 14.98327544 06
| Epoch (UTC): | 25 May 2026 12:11:48 |
| Eccentricity: | 0.0003550 |
| inclination: | 69.9993° |
| perigee height: | 570 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 230.7030° |
| argument of perigee: | 268.9645° |
| revolutions per day: | 14.98327544 |
| mean anomaly at epoch: | 91.1107° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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