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 68601U 26145.37551453 +.00000000 +00000-0 +95588-3 0 00003
2 68601 51.8630 287.7187 0011558 299.8762 60.1075 15.36195339 03
| Epoch (UTC): | 25 May 2026 09:00:44 |
| Eccentricity: | 0.0011558 |
| inclination: | 51.8630° |
| perigee height: | 449 km |
| apogee height: | 465 km |
| right ascension of ascending node: | 287.7187° |
| argument of perigee: | 299.8762° |
| revolutions per day: | 15.36195339 |
| mean anomaly at epoch: | 60.1075° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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