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 68605U 26145.58335647 +.00000000 +00000-0 +47069-3 0 00006
2 68605 97.2847 345.0140 0002082 83.3234 235.3176 15.49181028 02
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0002082 |
| inclination: | 97.2847° |
| perigee height: | 418 km |
| apogee height: | 421 km |
| right ascension of ascending node: | 345.0140° |
| argument of perigee: | 83.3234° |
| revolutions per day: | 15.49181028 |
| mean anomaly at epoch: | 235.3176° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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