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 63793U 26145.57823464 +.00000000 +00000-0 +80809-3 0 00006
2 63793 43.0001 338.0963 0000836 267.9879 92.0877 15.27589642 07
| Epoch (UTC): | 25 May 2026 13:52:39 |
| Eccentricity: | 0.0000836 |
| inclination: | 43.0001° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 338.0963° |
| argument of perigee: | 267.9879° |
| revolutions per day: | 15.27589642 |
| mean anomaly at epoch: | 92.0877° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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