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 68808U 26145.56189074 +.00000000 +00000-0 +13796-2 0 00009
2 68808 97.2849 352.2238 0001926 87.0509 273.0977 15.75266644 04
| Epoch (UTC): | 25 May 2026 13:29:07 |
| Eccentricity: | 0.0001926 |
| inclination: | 97.2849° |
| perigee height: | 343 km |
| apogee height: | 345 km |
| right ascension of ascending node: | 352.2238° |
| argument of perigee: | 87.0509° |
| revolutions per day: | 15.75266644 |
| mean anomaly at epoch: | 273.0977° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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