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 data is extracted from the following two-line orbital elements,
1 41917U 17003A 23146.68289943 .00000258 00000-0 84883-4 0 9998
2 41917 86.4015 195.5022 0002413 83.7141 276.4329 14.34219683333032
| Epoch (UTC): | 26 May 2023 16:23:22 |
| Eccentricity: | 0.0002413 |
| inclination: | 86.4015° |
| perigee height: | 776 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 195.5022° |
| argument of perigee: | 83.7141° |
| revolutions per day: | 14.34219683 |
| mean anomaly at epoch: | 276.4329° |
| orbit number at epoch: | 33303 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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