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 66786U 26145.46211235 +.00000000 +00000-0 +48871-3 0 00009
2 66786 97.5235 216.8749 0014272 203.8901 156.1662 14.98627776 06
| Epoch (UTC): | 25 May 2026 11:05:26 |
| Eccentricity: | 0.0014272 |
| inclination: | 97.5235° |
| perigee height: | 561 km |
| apogee height: | 581 km |
| right ascension of ascending node: | 216.8749° |
| argument of perigee: | 203.8901° |
| revolutions per day: | 14.98627776 |
| mean anomaly at epoch: | 156.1662° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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