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 41605U 16040G 24278.54986137 .00042675 00000-0 95573-3 0 9999
2 41605 97.1138 301.2979 0009076 43.7584 316.4383 15.43284639460835
| Epoch (UTC): | 04 October 2024 13:11:48 |
| Eccentricity: | 0.0009076 |
| inclination: | 97.1138° |
| perigee height: | 430 km |
| apogee height: | 442 km |
| right ascension of ascending node: | 301.2979° |
| argument of perigee: | 43.7584° |
| revolutions per day: | 15.43284639 |
| mean anomaly at epoch: | 316.4383° |
| orbit number at epoch: | 46083 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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