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 65768U 26145.50116661 +.00000000 +00000-0 +22809-3 0 00003
2 65768 51.8979 60.9291 0001138 72.5315 287.5772 14.79936945 01
| Epoch (UTC): | 25 May 2026 12:01:40 |
| Eccentricity: | 0.0001138 |
| inclination: | 51.8979° |
| perigee height: | 629 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 60.9291° |
| argument of perigee: | 72.5315° |
| revolutions per day: | 14.79936945 |
| mean anomaly at epoch: | 287.5772° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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