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 55920U 26145.25209845 +.00000000 +00000-0 +50400-4 0 00000
2 55920 69.9995 91.6122 0003023 267.4638 92.6175 14.98324340 03
| Epoch (UTC): | 25 May 2026 06:03:01 |
| Eccentricity: | 0.0003023 |
| inclination: | 69.9995° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 91.6122° |
| argument of perigee: | 267.4638° |
| revolutions per day: | 14.98324340 |
| mean anomaly at epoch: | 92.6175° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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