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 33591U 09005A 23092.25913616 .00000359 00000-0 21812-3 0 9998
2 33591 99.1096 136.9415 0014912 96.8887 263.3981 14.12723425729224
| Epoch (UTC): | 02 April 2023 06:13:09 |
| Eccentricity: | 0.0014912 |
| inclination: | 99.1096° |
| perigee height: | 839 km |
| apogee height: | 861 km |
| right ascension of ascending node: | 136.9415° |
| argument of perigee: | 96.8887° |
| revolutions per day: | 14.12723425 |
| mean anomaly at epoch: | 263.3981° |
| orbit number at epoch: | 72922 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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