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 66860U 26145.36251083 +.00000000 +00000-0 +41899-3 0 00009
2 66860 42.9983 270.2940 0000683 293.6824 66.3956 15.27555377 00
| Epoch (UTC): | 25 May 2026 08:42:00 |
| Eccentricity: | 0.0000683 |
| inclination: | 42.9983° |
| perigee height: | 483 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 270.2940° |
| argument of perigee: | 293.6824° |
| revolutions per day: | 15.27555377 |
| mean anomaly at epoch: | 66.3956° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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