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 00050U 60009B 24282.65139816 -.00000053 00000-0 30919-3 0 9991
2 00050 47.2311 275.4033 0113777 336.9791 22.5925 12.20147092862428
| Epoch (UTC): | 08 October 2024 15:38:00 |
| Eccentricity: | 0.0113777 |
| inclination: | 47.2311° |
| perigee height: | 1501 km |
| apogee height: | 1682 km |
| right ascension of ascending node: | 275.4033° |
| argument of perigee: | 336.9791° |
| revolutions per day: | 12.20147092 |
| mean anomaly at epoch: | 22.5925° |
| orbit number at epoch: | 86242 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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