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 41917U 26038.11673841 +.00000000 +00000-0 +13103-4 0 00007
2 41917 86.4023 142.9249 0001816 89.1298 271.0106 14.34217988 05
| Epoch (UTC): | 07 February 2026 02:48:06 |
| Eccentricity: | 0.0001816 |
| inclination: | 86.4023° |
| perigee height: | 776 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 142.9249° |
| argument of perigee: | 89.1298° |
| revolutions per day: | 14.34217988 |
| mean anomaly at epoch: | 271.0106° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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