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 23149.82247637 .00000253 00000-0 83253-4 0 9996
2 41917 86.4011 194.1922 0002346 83.4637 276.6826 14.34221246333485
| Epoch (UTC): | 29 May 2023 19:44:21 |
| Eccentricity: | 0.0002346 |
| inclination: | 86.4011° |
| perigee height: | 776 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 194.1922° |
| argument of perigee: | 83.4637° |
| revolutions per day: | 14.34221246 |
| mean anomaly at epoch: | 276.6826° |
| orbit number at epoch: | 33348 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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