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 68577U 26145.58335647 +.00000000 +00000-0 -31149-2 0 00006
2 68577 51.8972 290.7590 0003491 329.1191 354.9885 14.88911768 07
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0003491 |
| inclination: | 51.8972° |
| perigee height: | 599 km |
| apogee height: | 604 km |
| right ascension of ascending node: | 290.7590° |
| argument of perigee: | 329.1191° |
| revolutions per day: | 14.88911768 |
| mean anomaly at epoch: | 354.9885° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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