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 24252.78656904 .00005599 00000-0 22394-2 0 9993
2 00020 33.3470 70.4377 1648728 193.7788 161.1911 11.59659169409477
| Epoch (UTC): | 08 September 2024 18:52:39 |
| Eccentricity: | 0.1648728 |
| inclination: | 33.3470° |
| perigee height: | 507 km |
| apogee height: | 3226 km |
| right ascension of ascending node: | 70.4377° |
| argument of perigee: | 193.7788° |
| revolutions per day: | 11.59659169 |
| mean anomaly at epoch: | 161.1911° |
| orbit number at epoch: | 40947 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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