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 60924U 26145.51407332 +.00000000 +00000-0 +23916-4 0 00002
2 60924 53.1574 322.8928 0000891 79.2905 280.8213 15.69716175 04
| Epoch (UTC): | 25 May 2026 12:20:15 |
| Eccentricity: | 0.0000891 |
| inclination: | 53.1574° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 322.8928° |
| argument of perigee: | 79.2905° |
| revolutions per day: | 15.69716175 |
| mean anomaly at epoch: | 280.8213° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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