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 26073.59021720 +.00000000 +00000-0 +44432-4 0 00008
2 20855 98.8227 56.9196 0024720 44.8709 64.9400 14.09162238 00
| Epoch (UTC): | 14 March 2026 14:09:54 |
| Eccentricity: | 0.0024720 |
| inclination: | 98.8227° |
| perigee height: | 844 km |
| apogee height: | 880 km |
| right ascension of ascending node: | 56.9196° |
| argument of perigee: | 44.8709° |
| revolutions per day: | 14.09162238 |
| mean anomaly at epoch: | 64.9400° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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