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 68554U 26145.58335647 +.00000000 +00000-0 +13028-2 0 00006
2 68554 53.1593 4.8846 0000626 97.1275 315.1226 15.34372182 07
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0000626 |
| inclination: | 53.1593° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 4.8846° |
| argument of perigee: | 97.1275° |
| revolutions per day: | 15.34372182 |
| mean anomaly at epoch: | 315.1226° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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