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 19039U 88029B 23333.84276447 .00000762 00000-0 25457-3 0 9996
2 19039 74.0472 278.4703 0024607 229.2842 130.6176 14.38998658869724
| Epoch (UTC): | 29 November 2023 20:13:34 |
| Eccentricity: | 0.0024607 |
| inclination: | 74.0472° |
| perigee height: | 744 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 278.4703° |
| argument of perigee: | 229.2842° |
| revolutions per day: | 14.38998658 |
| mean anomaly at epoch: | 130.6176° |
| orbit number at epoch: | 86972 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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