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 59859U 26145.53694021 +.00000000 +00000-0 -60735-5 0 00004
2 59859 42.9991 207.9019 0001190 274.7760 85.2956 15.27576033 08
| Epoch (UTC): | 25 May 2026 12:53:11 |
| Eccentricity: | 0.0001190 |
| inclination: | 42.9991° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 207.9019° |
| argument of perigee: | 274.7760° |
| revolutions per day: | 15.27576033 |
| mean anomaly at epoch: | 85.2956° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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