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 31043U 99025BEM 24357.58282012 .00001391 00000-0 84289-3 0 9993
2 31043 98.7907 19.1359 0041167 283.9142 207.2238 14.07612582910289
| Epoch (UTC): | 22 December 2024 13:59:15 |
| Eccentricity: | 0.0041167 |
| inclination: | 98.7907° |
| perigee height: | 838 km |
| apogee height: | 897 km |
| right ascension of ascending node: | 19.1359° |
| argument of perigee: | 283.9142° |
| revolutions per day: | 14.07612582 |
| mean anomaly at epoch: | 207.2238° |
| orbit number at epoch: | 91028 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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