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 00045U 60007A 24250.47097065 .00001625 00000-0 41585-3 0 9993
2 00045 66.6923 274.9697 0259421 272.5102 84.6326 14.34895749286930
| Epoch (UTC): | 06 September 2024 11:18:11 |
| Eccentricity: | 0.0259421 |
| inclination: | 66.6923° |
| perigee height: | 590 km |
| apogee height: | 961 km |
| right ascension of ascending node: | 274.9697° |
| argument of perigee: | 272.5102° |
| revolutions per day: | 14.34895749 |
| mean anomaly at epoch: | 84.6326° |
| orbit number at epoch: | 28693 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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