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 24279U 96046C 19347.83175512 -.00000020 00000-0 16678-4 0 9990
2 24279 98.6941 188.6145 0300620 129.7719 244.5011 13.47132766146720
| Epoch (UTC): | 13 December 2019 19:57:43 |
| Eccentricity: | 0.0300620 |
| inclination: | 98.6941° |
| perigee height: | 858 km |
| apogee height: | 1307 km |
| right ascension of ascending node: | 188.6145° |
| argument of perigee: | 129.7719° |
| revolutions per day: | 13.47132766 |
| mean anomaly at epoch: | 244.5011° |
| orbit number at epoch: | 14672 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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