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 68079U 26145.50062269 +.00000000 +00000-0 +84582-3 0 00001
2 68079 53.1588 181.3468 0001169 81.8224 278.2911 15.34395678 06
| Epoch (UTC): | 25 May 2026 12:00:53 |
| Eccentricity: | 0.0001169 |
| inclination: | 53.1588° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 181.3468° |
| argument of perigee: | 81.8224° |
| revolutions per day: | 15.34395678 |
| mean anomaly at epoch: | 278.2911° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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