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 68817U 26145.29966558 +.00000000 +00000-0 +12886-2 0 00008
2 68817 97.2853 351.9680 0001642 75.5497 284.5950 15.75251455 01
| Epoch (UTC): | 25 May 2026 07:11:31 |
| Eccentricity: | 0.0001642 |
| inclination: | 97.2853° |
| perigee height: | 343 km |
| apogee height: | 345 km |
| right ascension of ascending node: | 351.9680° |
| argument of perigee: | 75.5497° |
| revolutions per day: | 15.75251455 |
| mean anomaly at epoch: | 284.5950° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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