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 26042.22039963 +.00000000 +00000-0 +10933-3 0 00003
2 41918 86.4019 141.1125 0002452 91.7814 268.3662 14.34219776 08
| Epoch (UTC): | 11 February 2026 05:17:22 |
| Eccentricity: | 0.0002452 |
| inclination: | 86.4019° |
| perigee height: | 776 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 141.1125° |
| argument of perigee: | 91.7814° |
| revolutions per day: | 14.34219776 |
| mean anomaly at epoch: | 268.3662° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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