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 26145.63002589 +.00000000 +00000-0 +60891-5 0 00005
2 41917 86.3950 97.9859 0002134 76.5880 283.5554 14.34217793 09
| Epoch (UTC): | 25 May 2026 15:07:14 |
| Eccentricity: | 0.0002134 |
| inclination: | 86.3950° |
| perigee height: | 776 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 97.9859° |
| argument of perigee: | 76.5880° |
| revolutions per day: | 14.34217793 |
| mean anomaly at epoch: | 283.5554° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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