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 59647U 26145.49823392 +.00000000 +00000-0 -65022-5 0 00003
2 59647 43.0040 66.4734 0000851 276.2850 83.7905 15.27581072 08
| Epoch (UTC): | 25 May 2026 11:57:27 |
| Eccentricity: | 0.0000851 |
| inclination: | 43.0040° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 66.4734° |
| argument of perigee: | 276.2850° |
| revolutions per day: | 15.27581072 |
| mean anomaly at epoch: | 83.7905° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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