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 26020.87122955 +.00000000 +00000-0 +35038-4 0 00008
2 41918 86.4015 150.0200 0002464 99.6700 260.4774 14.34218564 02
| Epoch (UTC): | 20 January 2026 20:54:34 |
| Eccentricity: | 0.0002464 |
| inclination: | 86.4015° |
| perigee height: | 776 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 150.0200° |
| argument of perigee: | 99.6700° |
| revolutions per day: | 14.34218564 |
| mean anomaly at epoch: | 260.4774° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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