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 20855U 26068.54901845 +.00000000 +00000-0 +11662-3 0 00000
2 20855 98.8225 51.9827 0024873 58.5509 51.5634 14.09160674 06
| Epoch (UTC): | 09 March 2026 13:10:35 |
| Eccentricity: | 0.0024873 |
| inclination: | 98.8225° |
| perigee height: | 844 km |
| apogee height: | 880 km |
| right ascension of ascending node: | 51.9827° |
| argument of perigee: | 58.5509° |
| revolutions per day: | 14.09160674 |
| mean anomaly at epoch: | 51.5634° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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