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 60454U 24147A 24341.38980119 .00051787 00000-0 13860-2 0 9998
2 60454 37.3826 322.9189 0005063 211.3736 148.6723 15.37042407 17238
| Epoch (UTC): | 06 December 2024 09:21:18 |
| Eccentricity: | 0.0005063 |
| inclination: | 37.3826° |
| perigee height: | 451 km |
| apogee height: | 458 km |
| right ascension of ascending node: | 322.9189° |
| argument of perigee: | 211.3736° |
| revolutions per day: | 15.37042407 |
| mean anomaly at epoch: | 148.6723° |
| orbit number at epoch: | 1723 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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