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 59606U 26145.55529683 +.00000000 +00000-0 +14598-4 0 00001
2 59606 43.0034 327.6670 0001427 279.8007 80.2683 15.27573474 02
| Epoch (UTC): | 25 May 2026 13:19:37 |
| Eccentricity: | 0.0001427 |
| inclination: | 43.0034° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 327.6670° |
| argument of perigee: | 279.8007° |
| revolutions per day: | 15.27573474 |
| mean anomaly at epoch: | 80.2683° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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