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 66161U 26145.47611691 +.00000000 +00000-0 +72455-3 0 00002
2 66161 53.1575 66.2242 0001020 43.3663 316.7418 15.30239594 09
| Epoch (UTC): | 25 May 2026 11:25:36 |
| Eccentricity: | 0.0001020 |
| inclination: | 53.1575° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 66.2242° |
| argument of perigee: | 43.3663° |
| revolutions per day: | 15.30239594 |
| mean anomaly at epoch: | 316.7418° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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