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 00020U 59007A 24254.76648113 .00005615 00000-0 22429-2 0 9994
2 00020 33.3485 63.3365 1648690 204.3541 146.9581 11.59682040409709
| Epoch (UTC): | 10 September 2024 18:23:43 |
| Eccentricity: | 0.1648690 |
| inclination: | 33.3485° |
| perigee height: | 507 km |
| apogee height: | 3226 km |
| right ascension of ascending node: | 63.3365° |
| argument of perigee: | 204.3541° |
| revolutions per day: | 11.59682040 |
| mean anomaly at epoch: | 146.9581° |
| orbit number at epoch: | 40970 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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