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 59164U 26144.97142781 +.00000000 +00000-0 +33785-3 0 00003
2 59164 43.0012 36.0760 0001397 249.9725 110.0976 15.27583360 01
| Epoch (UTC): | 24 May 2026 23:18:51 |
| Eccentricity: | 0.0001397 |
| inclination: | 43.0012° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 36.0760° |
| argument of perigee: | 249.9725° |
| revolutions per day: | 15.27583360 |
| mean anomaly at epoch: | 110.0976° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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