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 24276.69053129 .00000769 00000-0 26767-3 0 9992
2 41917 86.4021 348.6747 0002335 102.9015 257.2441 14.34221176403985
| Epoch (UTC): | 02 October 2024 16:34:21 |
| Eccentricity: | 0.0002335 |
| inclination: | 86.4021° |
| perigee height: | 776 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 348.6747° |
| argument of perigee: | 102.9015° |
| revolutions per day: | 14.34221176 |
| mean anomaly at epoch: | 257.2441° |
| orbit number at epoch: | 40398 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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