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 59161U 26145.41755596 +.00000000 +00000-0 +18567-3 0 00005
2 59161 43.0034 33.4088 0001590 289.9967 70.0713 15.27586515 02
| Epoch (UTC): | 25 May 2026 10:01:16 |
| Eccentricity: | 0.0001590 |
| inclination: | 43.0034° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 33.4088° |
| argument of perigee: | 289.9967° |
| revolutions per day: | 15.27586515 |
| mean anomaly at epoch: | 70.0713° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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