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 65979U 26145.60306949 +.00000000 +00000-0 -18528-1 0 00000
2 65979 81.3018 232.5133 0002593 249.2407 110.8472 13.85012206 06
| Epoch (UTC): | 25 May 2026 14:28:25 |
| Eccentricity: | 0.0002593 |
| inclination: | 81.3018° |
| perigee height: | 944 km |
| apogee height: | 948 km |
| right ascension of ascending node: | 232.5133° |
| argument of perigee: | 249.2407° |
| revolutions per day: | 13.85012206 |
| mean anomaly at epoch: | 110.8472° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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