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 66584U 26145.64661770 +.00000000 +00000-0 +59110-3 0 00006
2 66584 43.0061 272.0677 0000868 296.7985 63.2778 15.27586820 01
| Epoch (UTC): | 25 May 2026 15:31:07 |
| Eccentricity: | 0.0000868 |
| inclination: | 43.0061° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 272.0677° |
| argument of perigee: | 296.7985° |
| revolutions per day: | 15.27586820 |
| mean anomaly at epoch: | 63.2778° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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