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 24279.19384249 .00022464 00000-0 17073-2 0 9991
2 31702 63.3264 324.1299 0520280 34.1884 329.1558 14.32905587 21273
| Epoch (UTC): | 05 October 2024 04:39:07 |
| Eccentricity: | 0.0520280 |
| inclination: | 63.3264° |
| perigee height: | 409 km |
| apogee height: | 1154 km |
| right ascension of ascending node: | 324.1299° |
| argument of perigee: | 34.1884° |
| revolutions per day: | 14.32905587 |
| mean anomaly at epoch: | 329.1558° |
| orbit number at epoch: | 2127 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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