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 60596U 26145.45536293 +.00000000 +00000-0 +52715-4 0 00008
2 60596 53.1625 309.8110 0001367 84.4584 275.6574 15.34390325 03
| Epoch (UTC): | 25 May 2026 10:55:43 |
| Eccentricity: | 0.0001367 |
| inclination: | 53.1625° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 309.8110° |
| argument of perigee: | 84.4584° |
| revolutions per day: | 15.34390325 |
| mean anomaly at epoch: | 275.6574° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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