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 24262.51481537 .00003631 00000-0 14394-2 0 9999
2 00020 33.3563 35.5465 1648720 245.7271 96.2681 11.59755592410603
| Epoch (UTC): | 18 September 2024 12:21:20 |
| Eccentricity: | 0.1648720 |
| inclination: | 33.3563° |
| perigee height: | 507 km |
| apogee height: | 3225 km |
| right ascension of ascending node: | 35.5465° |
| argument of perigee: | 245.7271° |
| revolutions per day: | 11.59755592 |
| mean anomaly at epoch: | 96.2681° |
| orbit number at epoch: | 41060 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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