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 68085U 26145.46016975 +.00000000 +00000-0 +45095-3 0 00002
2 68085 53.1581 179.6551 0000943 89.3223 270.7888 15.34403763 05
| Epoch (UTC): | 25 May 2026 11:02:38 |
| Eccentricity: | 0.0000943 |
| inclination: | 53.1581° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 179.6551° |
| argument of perigee: | 89.3223° |
| revolutions per day: | 15.34403763 |
| mean anomaly at epoch: | 270.7888° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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