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 55945U 26145.27308359 +.00000000 +00000-0 -36141-4 0 00006
2 55945 69.9998 91.2845 0003031 266.3029 93.7783 14.98336035 03
| Epoch (UTC): | 25 May 2026 06:33:14 |
| Eccentricity: | 0.0003031 |
| inclination: | 69.9998° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 91.2845° |
| argument of perigee: | 266.3029° |
| revolutions per day: | 14.98336035 |
| mean anomaly at epoch: | 93.7783° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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