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 60544U 26145.59365873 +.00000000 +00000-0 +60458-3 0 00002
2 60544 97.6771 219.0601 0005124 142.6299 217.5278 14.92493713 07
| Epoch (UTC): | 25 May 2026 14:14:52 |
| Eccentricity: | 0.0005124 |
| inclination: | 97.6771° |
| perigee height: | 587 km |
| apogee height: | 594 km |
| right ascension of ascending node: | 219.0601° |
| argument of perigee: | 142.6299° |
| revolutions per day: | 14.92493713 |
| mean anomaly at epoch: | 217.5278° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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