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 31194U 99025BJY 24358.09703786 .00005375 00000-0 19021-2 0 9990
2 31194 98.9982 226.7480 0059107 238.0767 121.4660 14.34033389920389
| Epoch (UTC): | 23 December 2024 02:19:44 |
| Eccentricity: | 0.0059107 |
| inclination: | 98.9982° |
| perigee height: | 736 km |
| apogee height: | 820 km |
| right ascension of ascending node: | 226.7480° |
| argument of perigee: | 238.0767° |
| revolutions per day: | 14.34033389 |
| mean anomaly at epoch: | 121.4660° |
| orbit number at epoch: | 92038 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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