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 41918U 26145.61734168 +.00000000 +00000-0 +15172-5 0 00001
2 41918 86.3950 97.8909 0002589 85.5752 274.5739 14.34217731 04
| Epoch (UTC): | 25 May 2026 14:48:58 |
| Eccentricity: | 0.0002589 |
| inclination: | 86.3950° |
| perigee height: | 776 km |
| apogee height: | 780 km |
| right ascension of ascending node: | 97.8909° |
| argument of perigee: | 85.5752° |
| revolutions per day: | 14.34217731 |
| mean anomaly at epoch: | 274.5739° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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