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 68786U 26145.58335647 +.00000000 +00000-0 -22342-1 0 00002
2 68786 97.2849 182.4739 0001971 94.6886 127.3914 15.63945822 01
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001971 |
| inclination: | 97.2849° |
| perigee height: | 375 km |
| apogee height: | 378 km |
| right ascension of ascending node: | 182.4739° |
| argument of perigee: | 94.6886° |
| revolutions per day: | 15.63945822 |
| mean anomaly at epoch: | 127.3914° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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