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 24726U 97006B 23270.48025029 .00000017 00000-0 36618-4 0 9993
2 24726 82.6043 174.7723 0004752 169.2237 190.8956 12.61358167225192
| Epoch (UTC): | 27 September 2023 11:31:33 |
| Eccentricity: | 0.0004752 |
| inclination: | 82.6043° |
| perigee height: | 1413 km |
| apogee height: | 1421 km |
| right ascension of ascending node: | 174.7723° |
| argument of perigee: | 169.2237° |
| revolutions per day: | 12.61358167 |
| mean anomaly at epoch: | 190.8956° |
| orbit number at epoch: | 22519 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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