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 68044U 26145.03476904 +.00000000 +00000-0 +36431-3 0 00006
2 68044 53.1585 53.3880 0001351 101.0745 259.0409 15.34401980 00
| Epoch (UTC): | 25 May 2026 00:50:04 |
| Eccentricity: | 0.0001351 |
| inclination: | 53.1585° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 53.3880° |
| argument of perigee: | 101.0745° |
| revolutions per day: | 15.34401980 |
| mean anomaly at epoch: | 259.0409° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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