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 23432U 94083B 24282.59587157 .00001057 00000-0 38736-3 0 9996
2 23432 74.0303 93.5986 0005131 5.6525 58.0481 14.34065253558755
| Epoch (UTC): | 08 October 2024 14:18:03 |
| Eccentricity: | 0.0005131 |
| inclination: | 74.0303° |
| perigee height: | 774 km |
| apogee height: | 782 km |
| right ascension of ascending node: | 93.5986° |
| argument of perigee: | 5.6525° |
| revolutions per day: | 14.34065253 |
| mean anomaly at epoch: | 58.0481° |
| orbit number at epoch: | 55875 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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