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 24276.34488074 -.00000030 00000-0 51802-3 0 9992
2 00050 47.2316 294.9786 0113872 318.1944 41.0191 12.20146564861650
| Epoch (UTC): | 02 October 2024 08:16:37 |
| Eccentricity: | 0.0113872 |
| inclination: | 47.2316° |
| perigee height: | 1501 km |
| apogee height: | 1682 km |
| right ascension of ascending node: | 294.9786° |
| argument of perigee: | 318.1944° |
| revolutions per day: | 12.20146564 |
| mean anomaly at epoch: | 41.0191° |
| orbit number at epoch: | 86165 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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