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 68866U 26144.99874495 +.00000000 +00000-0 +95753-3 0 00001
2 68866 51.8836 354.3818 0003362 194.3993 165.6900 15.38411050 06
| Epoch (UTC): | 24 May 2026 23:58:11 |
| Eccentricity: | 0.0003362 |
| inclination: | 51.8836° |
| perigee height: | 449 km |
| apogee height: | 453 km |
| right ascension of ascending node: | 354.3818° |
| argument of perigee: | 194.3993° |
| revolutions per day: | 15.38411050 |
| mean anomaly at epoch: | 165.6900° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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