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 66990U 26144.93685566 +.00000000 +00000-0 +00000-0 0 00008
2 66990 1.5854 286.2889 0001874 348.9360 11.1231 1.00274659 04
| Epoch (UTC): | 24 May 2026 22:29:04 |
| Eccentricity: | 0.0001874 |
| inclination: | 1.5854° |
| perigee height: | 35778 km |
| apogee height: | 35794 km |
| right ascension of ascending node: | 286.2889° |
| argument of perigee: | 348.9360° |
| revolutions per day: | 1.00274659 |
| mean anomaly at epoch: | 11.1231° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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