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 17129U 86019Y 24358.11853262 .00000433 00000-0 19876-3 0 9998
2 17129 98.3419 24.6717 0032274 339.9588 87.4244 14.25735698929825
| Epoch (UTC): | 23 December 2024 02:50:41 |
| Eccentricity: | 0.0032274 |
| inclination: | 98.3419° |
| perigee height: | 783 km |
| apogee height: | 829 km |
| right ascension of ascending node: | 24.6717° |
| argument of perigee: | 339.9588° |
| revolutions per day: | 14.25735698 |
| mean anomaly at epoch: | 87.4244° |
| orbit number at epoch: | 92982 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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