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 24280.19431150 -.00000081 00000-0 42860-4 0 9994
2 00050 47.2311 283.0302 0113818 329.6601 29.7635 12.20146925862125
| Epoch (UTC): | 06 October 2024 04:39:48 |
| Eccentricity: | 0.0113818 |
| inclination: | 47.2311° |
| perigee height: | 1501 km |
| apogee height: | 1682 km |
| right ascension of ascending node: | 283.0302° |
| argument of perigee: | 329.6601° |
| revolutions per day: | 12.20146925 |
| mean anomaly at epoch: | 29.7635° |
| orbit number at epoch: | 86212 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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