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 00051U 60009C 24250.24572813 .00000007 00000-0 89642-3 0 9995
2 00051 47.2106 257.3634 0105500 66.3816 294.8008 12.18332313852057
| Epoch (UTC): | 06 September 2024 05:53:50 |
| Eccentricity: | 0.0105500 |
| inclination: | 47.2106° |
| perigee height: | 1515 km |
| apogee height: | 1684 km |
| right ascension of ascending node: | 257.3634° |
| argument of perigee: | 66.3816° |
| revolutions per day: | 12.18332313 |
| mean anomaly at epoch: | 294.8008° |
| orbit number at epoch: | 85205 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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