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 60594U 26145.46167287 +.00000000 +00000-0 +26748-4 0 00007
2 60594 53.1618 309.8485 0001103 78.7991 281.3135 15.34391454 05
| Epoch (UTC): | 25 May 2026 11:04:48 |
| Eccentricity: | 0.0001103 |
| inclination: | 53.1618° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 309.8485° |
| argument of perigee: | 78.7991° |
| revolutions per day: | 15.34391454 |
| mean anomaly at epoch: | 281.3135° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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