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 68733U 26145.58335647 +.00000000 +00000-0 +17038-2 0 00000
2 68733 97.2853 9.2746 0002030 72.4147 351.3498 15.49145668 03
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0002030 |
| inclination: | 97.2853° |
| perigee height: | 418 km |
| apogee height: | 421 km |
| right ascension of ascending node: | 9.2746° |
| argument of perigee: | 72.4147° |
| revolutions per day: | 15.49145668 |
| mean anomaly at epoch: | 351.3498° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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