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 54166U 26145.38160098 +.00000000 +00000-0 +19503-4 0 00000
2 54166 53.2128 19.9653 0001290 122.0406 238.0711 15.08840274 06
| Epoch (UTC): | 25 May 2026 09:09:30 |
| Eccentricity: | 0.0001290 |
| inclination: | 53.2128° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 19.9653° |
| argument of perigee: | 122.0406° |
| revolutions per day: | 15.08840274 |
| mean anomaly at epoch: | 238.0711° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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