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 31702U 07027B 24276.54179569 .00019482 00000-0 14877-2 0 9999
2 31702 63.3275 332.0838 0520370 34.1558 329.1862 14.32800905 20893
| Epoch (UTC): | 02 October 2024 13:00:11 |
| Eccentricity: | 0.0520370 |
| inclination: | 63.3275° |
| perigee height: | 410 km |
| apogee height: | 1155 km |
| right ascension of ascending node: | 332.0838° |
| argument of perigee: | 34.1558° |
| revolutions per day: | 14.32800905 |
| mean anomaly at epoch: | 329.1862° |
| orbit number at epoch: | 2089 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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