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 68504U 26145.37328494 +.00000000 +00000-0 +23317-3 0 00003
2 68504 97.7615 104.0061 0003473 66.9239 293.2346 14.91961541 04
| Epoch (UTC): | 25 May 2026 08:57:31 |
| Eccentricity: | 0.0003473 |
| inclination: | 97.7615° |
| perigee height: | 589 km |
| apogee height: | 594 km |
| right ascension of ascending node: | 104.0061° |
| argument of perigee: | 66.9239° |
| revolutions per day: | 14.91961541 |
| mean anomaly at epoch: | 293.2346° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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