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 26039.57929369 +.00000000 +00000-0 -69862-6 0 00001
2 20855 98.8177 23.6240 0024608 137.1374 332.2131 14.09154730 04
| Epoch (UTC): | 08 February 2026 13:54:10 |
| Eccentricity: | 0.0024608 |
| inclination: | 98.8177° |
| perigee height: | 844 km |
| apogee height: | 880 km |
| right ascension of ascending node: | 23.6240° |
| argument of perigee: | 137.1374° |
| revolutions per day: | 14.09154730 |
| mean anomaly at epoch: | 332.2131° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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