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 60593U 26145.43642486 +.00000000 +00000-0 +43915-4 0 00007
2 60593 53.1602 309.6934 0001065 94.1473 265.9651 15.34391344 07
| Epoch (UTC): | 25 May 2026 10:28:27 |
| Eccentricity: | 0.0001065 |
| inclination: | 53.1602° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 309.6934° |
| argument of perigee: | 94.1473° |
| revolutions per day: | 15.34391344 |
| mean anomaly at epoch: | 265.9651° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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