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 26065.43529219 +.00000000 +00000-0 +43103-4 0 00002
2 20855 98.8218 48.9336 0024925 66.9379 96.1007 14.09160030 00
| Epoch (UTC): | 06 March 2026 10:26:49 |
| Eccentricity: | 0.0024925 |
| inclination: | 98.8218° |
| perigee height: | 844 km |
| apogee height: | 880 km |
| right ascension of ascending node: | 48.9336° |
| argument of perigee: | 66.9379° |
| revolutions per day: | 14.09160030 |
| mean anomaly at epoch: | 96.1007° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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