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 31667U 99025CBZ 24354.36456716 .00000993 00000-0 45713-3 0 9998
2 31667 99.1152 188.1529 0052018 33.5270 326.9181 14.22836993508956
| Epoch (UTC): | 19 December 2024 08:44:58 |
| Eccentricity: | 0.0052018 |
| inclination: | 99.1152° |
| perigee height: | 778 km |
| apogee height: | 853 km |
| right ascension of ascending node: | 188.1529° |
| argument of perigee: | 33.5270° |
| revolutions per day: | 14.22836993 |
| mean anomaly at epoch: | 326.9181° |
| orbit number at epoch: | 50895 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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