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 31293U 99025BPB 24276.75863964 .00001111 00000-0 40506-3 0 9994
2 31293 98.4396 291.6565 0128398 94.0198 267.5673 14.30446403590105
| Epoch (UTC): | 02 October 2024 18:12:26 |
| Eccentricity: | 0.0128398 |
| inclination: | 98.4396° |
| perigee height: | 698 km |
| apogee height: | 882 km |
| right ascension of ascending node: | 291.6565° |
| argument of perigee: | 94.0198° |
| revolutions per day: | 14.30446403 |
| mean anomaly at epoch: | 267.5673° |
| orbit number at epoch: | 59010 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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