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 55790U 26145.37647602 +.00000000 +00000-0 +92874-4 0 00006
2 55790 69.9998 11.0823 0002875 269.6532 90.4298 14.98326949 05
| Epoch (UTC): | 25 May 2026 09:02:07 |
| Eccentricity: | 0.0002875 |
| inclination: | 69.9998° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 11.0823° |
| argument of perigee: | 269.6532° |
| revolutions per day: | 14.98326949 |
| mean anomaly at epoch: | 90.4298° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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