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 66793U 26145.42699639 +.00000000 +00000-0 +42976-3 0 00001
2 66793 42.9993 41.1179 0000186 357.0723 3.0127 15.27592820 08
| Epoch (UTC): | 25 May 2026 10:14:52 |
| Eccentricity: | 0.0000186 |
| inclination: | 42.9993° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 41.1179° |
| argument of perigee: | 357.0723° |
| revolutions per day: | 15.27592820 |
| mean anomaly at epoch: | 3.0127° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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