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 68779U 26143.63524617 +.00000000 +00000-0 +16805-2 0 00002
2 68779 97.2843 180.4367 0001205 12.0261 348.1033 15.75315605 01
| Epoch (UTC): | 23 May 2026 15:14:45 |
| Eccentricity: | 0.0001205 |
| inclination: | 97.2843° |
| perigee height: | 343 km |
| apogee height: | 345 km |
| right ascension of ascending node: | 180.4367° |
| argument of perigee: | 12.0261° |
| revolutions per day: | 15.75315605 |
| mean anomaly at epoch: | 348.1033° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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