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 39019U 12068A 24358.49878877 .00001037 00000-0 23300-3 0 9991
2 39019 98.1791 70.2271 0001266 89.5687 270.5657 14.58537989642032
| Epoch (UTC): | 23 December 2024 11:58:15 |
| Eccentricity: | 0.0001266 |
| inclination: | 98.1791° |
| perigee height: | 697 km |
| apogee height: | 699 km |
| right ascension of ascending node: | 70.2271° |
| argument of perigee: | 89.5687° |
| revolutions per day: | 14.58537989 |
| mean anomaly at epoch: | 270.5657° |
| orbit number at epoch: | 64203 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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