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 27432U 02024C 23150.07200873 .00000046 00000-0 47568-4 0 9998
2 27432 99.0237 184.4595 0050651 18.8957 35.1567 14.14213542 85817
| Epoch (UTC): | 30 May 2023 01:43:41 |
| Eccentricity: | 0.0050651 |
| inclination: | 99.0237° |
| perigee height: | 808 km |
| apogee height: | 881 km |
| right ascension of ascending node: | 184.4595° |
| argument of perigee: | 18.8957° |
| revolutions per day: | 14.14213542 |
| mean anomaly at epoch: | 35.1567° |
| orbit number at epoch: | 8581 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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