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 25544U 26105.87667374 +.00000000 +00000-0 +10765-3 0 00007
2 25544 51.6326 248.4785 0006599 317.1782 42.8691 15.48928061 05
| Epoch (UTC): | 15 April 2026 21:02:24 |
| Eccentricity: | 0.0006599 |
| inclination: | 51.6326° |
| perigee height: | 415 km |
| apogee height: | 424 km |
| right ascension of ascending node: | 248.4785° |
| argument of perigee: | 317.1782° |
| revolutions per day: | 15.48928061 |
| mean anomaly at epoch: | 42.8691° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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