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 68604U 26145.58335647 +.00000000 +00000-0 -14546-1 0 00008
2 68604 97.2846 345.0142 0001908 79.0530 238.1403 15.49660383 09
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001908 |
| inclination: | 97.2846° |
| perigee height: | 416 km |
| apogee height: | 419 km |
| right ascension of ascending node: | 345.0142° |
| argument of perigee: | 79.0530° |
| revolutions per day: | 15.49660383 |
| mean anomaly at epoch: | 238.1403° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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