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 23705U 95058B 24284.44736455 .00000127 00000-0 89413-4 0 9991
2 23705 71.0224 181.9171 0012939 195.6847 164.3877 14.15385432494949
| Epoch (UTC): | 10 October 2024 10:44:12 |
| Eccentricity: | 0.0012939 |
| inclination: | 71.0224° |
| perigee height: | 831 km |
| apogee height: | 850 km |
| right ascension of ascending node: | 181.9171° |
| argument of perigee: | 195.6847° |
| revolutions per day: | 14.15385432 |
| mean anomaly at epoch: | 164.3877° |
| orbit number at epoch: | 49494 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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