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 43055U 26145.13889047 +.00000000 +00000-0 +00000-0 0 00008
2 43055 55.0795 222.1411 0003324 263.2184 96.7978 1.70474628 06
| Epoch (UTC): | 25 May 2026 03:20:00 |
| Eccentricity: | 0.0003324 |
| inclination: | 55.0795° |
| perigee height: | 23212 km |
| apogee height: | 23232 km |
| right ascension of ascending node: | 222.1411° |
| argument of perigee: | 263.2184° |
| revolutions per day: | 1.70474628 |
| mean anomaly at epoch: | 96.7978° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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