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 23405U 94077B 24277.18625621 .00000161 00000-0 10714-3 0 9998
2 23405 70.9855 11.6441 0004772 254.1788 105.8809 14.15433383542560
| Epoch (UTC): | 03 October 2024 04:28:12 |
| Eccentricity: | 0.0004772 |
| inclination: | 70.9855° |
| perigee height: | 837 km |
| apogee height: | 844 km |
| right ascension of ascending node: | 11.6441° |
| argument of perigee: | 254.1788° |
| revolutions per day: | 14.15433383 |
| mean anomaly at epoch: | 105.8809° |
| orbit number at epoch: | 54256 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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