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 60927U 26145.49444808 +.00000000 +00000-0 +23861-4 0 00000
2 60927 53.1583 322.7647 0000493 42.4346 317.6710 15.69718624 05
| Epoch (UTC): | 25 May 2026 11:52:00 |
| Eccentricity: | 0.0000493 |
| inclination: | 53.1583° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 322.7647° |
| argument of perigee: | 42.4346° |
| revolutions per day: | 15.69718624 |
| mean anomaly at epoch: | 317.6710° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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