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 66249U 26145.66429807 +.00000000 +00000-0 +77903-3 0 00009
2 66249 53.1594 286.2109 0001170 7.4430 352.6588 15.30207987 00
| Epoch (UTC): | 25 May 2026 15:56:35 |
| Eccentricity: | 0.0001170 |
| inclination: | 53.1594° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 286.2109° |
| argument of perigee: | 7.4430° |
| revolutions per day: | 15.30207987 |
| mean anomaly at epoch: | 352.6588° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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