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 68599U 26145.41633196 +.00000000 +00000-0 +72607-3 0 00006
2 68599 51.8670 287.2766 0010061 303.6426 56.3601 15.37346255 08
| Epoch (UTC): | 25 May 2026 09:59:31 |
| Eccentricity: | 0.0010061 |
| inclination: | 51.8670° |
| perigee height: | 447 km |
| apogee height: | 461 km |
| right ascension of ascending node: | 287.2766° |
| argument of perigee: | 303.6426° |
| revolutions per day: | 15.37346255 |
| mean anomaly at epoch: | 56.3601° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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