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 23604U 95032B 24284.57927170 .00000170 00000-0 16361-3 0 9990
2 23604 82.9047 328.4275 0024053 2.4396 357.6873 13.74456668467855
| Epoch (UTC): | 10 October 2024 13:54:09 |
| Eccentricity: | 0.0024053 |
| inclination: | 82.9047° |
| perigee height: | 966 km |
| apogee height: | 1001 km |
| right ascension of ascending node: | 328.4275° |
| argument of perigee: | 2.4396° |
| revolutions per day: | 13.74456668 |
| mean anomaly at epoch: | 357.6873° |
| orbit number at epoch: | 46785 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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