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 41859U 26144.86855127 +.00000000 +00000-0 +00000-0 0 00009
2 41859 55.4851 101.7309 0005705 323.8693 36.0515 1.70473749 01
| Epoch (UTC): | 24 May 2026 20:50:42 |
| Eccentricity: | 0.0005705 |
| inclination: | 55.4851° |
| perigee height: | 23205 km |
| apogee height: | 23239 km |
| right ascension of ascending node: | 101.7309° |
| argument of perigee: | 323.8693° |
| revolutions per day: | 1.70473749 |
| mean anomaly at epoch: | 36.0515° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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