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 68791U 26139.48610788 +.00000000 +00000-0 +00000-0 0 00007
2 68791 54.9639 208.9229 0005154 271.7816 81.6763 2.00570690 08
| Epoch (UTC): | 19 May 2026 11:39:59 |
| Eccentricity: | 0.0005154 |
| inclination: | 54.9639° |
| perigee height: | 20168 km |
| apogee height: | 20195 km |
| right ascension of ascending node: | 208.9229° |
| argument of perigee: | 271.7816° |
| revolutions per day: | 2.00570690 |
| mean anomaly at epoch: | 81.6763° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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