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 66717U 26144.64430828 +.00000000 +00000-0 +23255-3 0 00002
2 66717 97.4209 218.8722 0001987 72.4948 287.6505 15.20702790 05
| Epoch (UTC): | 24 May 2026 15:27:48 |
| Eccentricity: | 0.0001987 |
| inclination: | 97.4209° |
| perigee height: | 502 km |
| apogee height: | 505 km |
| right ascension of ascending node: | 218.8722° |
| argument of perigee: | 72.4948° |
| revolutions per day: | 15.20702790 |
| mean anomaly at epoch: | 287.6505° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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