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 66780U 26145.15186010 +.00000000 +00000-0 +16391-3 0 00003
2 66780 97.4180 218.8854 0004185 190.8776 169.2369 15.18706281 05
| Epoch (UTC): | 25 May 2026 03:38:40 |
| Eccentricity: | 0.0004185 |
| inclination: | 97.4180° |
| perigee height: | 507 km |
| apogee height: | 513 km |
| right ascension of ascending node: | 218.8854° |
| argument of perigee: | 190.8776° |
| revolutions per day: | 15.18706281 |
| mean anomaly at epoch: | 169.2369° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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