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 66722U 26145.61764065 +.00000000 +00000-0 +24698-3 0 00001
2 66722 97.4186 219.7966 0002311 56.3483 303.7973 15.20741917 05
| Epoch (UTC): | 25 May 2026 14:49:24 |
| Eccentricity: | 0.0002311 |
| inclination: | 97.4186° |
| perigee height: | 502 km |
| apogee height: | 505 km |
| right ascension of ascending node: | 219.7966° |
| argument of perigee: | 56.3483° |
| revolutions per day: | 15.20741917 |
| mean anomaly at epoch: | 303.7973° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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