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 55775U 26145.38905462 +.00000000 +00000-0 -35324-3 0 00008
2 55775 70.0009 31.0041 0002616 264.2055 95.8806 14.98352718 09
| Epoch (UTC): | 25 May 2026 09:20:14 |
| Eccentricity: | 0.0002616 |
| inclination: | 70.0009° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 31.0041° |
| argument of perigee: | 264.2055° |
| revolutions per day: | 14.98352718 |
| mean anomaly at epoch: | 95.8806° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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