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 26038.80174764 +.00000000 +00000-0 +13747-3 0 00007
2 41918 86.4020 142.5393 0002507 93.1366 267.0117 14.34219474 07
| Epoch (UTC): | 07 February 2026 19:14:30 |
| Eccentricity: | 0.0002507 |
| inclination: | 86.4020° |
| perigee height: | 776 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 142.5393° |
| argument of perigee: | 93.1366° |
| revolutions per day: | 14.34219474 |
| mean anomaly at epoch: | 267.0117° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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