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 41634U 26069.86760942 +.00000000 +00000-0 +11839-3 0 00001
2 41634 75.0003 105.0518 0008670 273.0516 86.9681 14.93233938 03
| Epoch (UTC): | 10 March 2026 20:49:21 |
| Eccentricity: | 0.0008670 |
| inclination: | 75.0003° |
| perigee height: | 582 km |
| apogee height: | 594 km |
| right ascension of ascending node: | 105.0518° |
| argument of perigee: | 273.0516° |
| revolutions per day: | 14.93233938 |
| mean anomaly at epoch: | 86.9681° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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