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 41873U 16062E 24200.55473233 .14265010 12672-4 19722-3 0 9993
2 41873 51.6369 255.9023 0003857 291.3520 68.7099 16.48908038427151
| Epoch (UTC): | 18 July 2024 13:18:48 |
| Eccentricity: | 0.0003857 |
| inclination: | 51.6369° |
| perigee height: | 140 km |
| apogee height: | 145 km |
| right ascension of ascending node: | 255.9023° |
| argument of perigee: | 291.3520° |
| revolutions per day: | 16.48908038 |
| mean anomaly at epoch: | 68.7099° |
| orbit number at epoch: | 42715 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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