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 26040.76794218 +.00000000 +00000-0 -15342-4 0 00001
2 41917 86.4022 141.8186 0001682 91.5980 268.5408 14.34217430 06
| Epoch (UTC): | 09 February 2026 18:25:50 |
| Eccentricity: | 0.0001682 |
| inclination: | 86.4022° |
| perigee height: | 776 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 141.8186° |
| argument of perigee: | 91.5980° |
| revolutions per day: | 14.34217430 |
| mean anomaly at epoch: | 268.5408° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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