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 23159.52030508 .00000303 00000-0 10104-3 0 9991
2 41917 86.4002 190.1451 0002140 84.7015 275.4425 14.34217248334877
| Epoch (UTC): | 08 June 2023 12:29:14 |
| Eccentricity: | 0.0002140 |
| inclination: | 86.4002° |
| perigee height: | 776 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 190.1451° |
| argument of perigee: | 84.7015° |
| revolutions per day: | 14.34217248 |
| mean anomaly at epoch: | 275.4425° |
| orbit number at epoch: | 33487 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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