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 68598U 26144.82598325 +.00000000 +00000-0 +74328-3 0 00005
2 68598 51.8668 290.0661 0009328 301.3869 58.6204 15.37643717 07
| Epoch (UTC): | 24 May 2026 19:49:24 |
| Eccentricity: | 0.0009328 |
| inclination: | 51.8668° |
| perigee height: | 447 km |
| apogee height: | 459 km |
| right ascension of ascending node: | 290.0661° |
| argument of perigee: | 301.3869° |
| revolutions per day: | 15.37643717 |
| mean anomaly at epoch: | 58.6204° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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