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 26064.99082645 +.00000000 +00000-0 +20614-4 0 00001
2 20855 98.8218 48.4985 0024929 68.1406 1.3881 14.09159840 09
| Epoch (UTC): | 05 March 2026 23:46:47 |
| Eccentricity: | 0.0024929 |
| inclination: | 98.8218° |
| perigee height: | 844 km |
| apogee height: | 880 km |
| right ascension of ascending node: | 48.4985° |
| argument of perigee: | 68.1406° |
| revolutions per day: | 14.09159840 |
| mean anomaly at epoch: | 1.3881° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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