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 50473U 21132E 24358.23633625 .00000115 00000-0 26226-3 0 9998
2 50473 87.9106 113.6138 0001825 100.7728 259.3609 13.17648864148168
| Epoch (UTC): | 23 December 2024 05:40:19 |
| Eccentricity: | 0.0001825 |
| inclination: | 87.9106° |
| perigee height: | 1192 km |
| apogee height: | 1195 km |
| right ascension of ascending node: | 113.6138° |
| argument of perigee: | 100.7728° |
| revolutions per day: | 13.17648864 |
| mean anomaly at epoch: | 259.3609° |
| orbit number at epoch: | 14816 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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