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 26064.57245787 +.00000000 +00000-0 +16774-4 0 00005
2 20855 98.8217 48.0888 0024945 69.2854 39.0499 14.09159797 07
| Epoch (UTC): | 05 March 2026 13:44:20 |
| Eccentricity: | 0.0024945 |
| inclination: | 98.8217° |
| perigee height: | 844 km |
| apogee height: | 880 km |
| right ascension of ascending node: | 48.0888° |
| argument of perigee: | 69.2854° |
| revolutions per day: | 14.09159797 |
| mean anomaly at epoch: | 39.0499° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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