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 55290U 26145.56615764 +.00000000 +00000-0 +16058-4 0 00006
2 55290 69.9986 190.6563 0003690 267.4446 92.6290 14.98332622 09
| Epoch (UTC): | 25 May 2026 13:35:16 |
| Eccentricity: | 0.0003690 |
| inclination: | 69.9986° |
| perigee height: | 569 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 190.6563° |
| argument of perigee: | 267.4446° |
| revolutions per day: | 14.98332622 |
| mean anomaly at epoch: | 92.6290° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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