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 26039.50842601 +.00000000 +00000-0 +13668-5 0 00008
2 20855 98.8177 23.5546 0024606 137.3339 332.7078 14.09154752 02
| Epoch (UTC): | 08 February 2026 12:12:08 |
| Eccentricity: | 0.0024606 |
| inclination: | 98.8177° |
| perigee height: | 844 km |
| apogee height: | 880 km |
| right ascension of ascending node: | 23.5546° |
| argument of perigee: | 137.3339° |
| revolutions per day: | 14.09154752 |
| mean anomaly at epoch: | 332.7078° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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