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 60511U 26145.61379380 +.00000000 +00000-0 +92818-3 0 00002
2 60511 97.3826 232.3101 0002295 30.2404 329.8980 15.50077563 01
| Epoch (UTC): | 25 May 2026 14:43:51 |
| Eccentricity: | 0.0002295 |
| inclination: | 97.3826° |
| perigee height: | 415 km |
| apogee height: | 418 km |
| right ascension of ascending node: | 232.3101° |
| argument of perigee: | 30.2404° |
| revolutions per day: | 15.50077563 |
| mean anomaly at epoch: | 329.8980° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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