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 33499U 09002H 23151.18879535 .00001113 00000-0 16533-3 0 9994
2 33499 98.1752 43.2876 0007390 285.1659 74.8733 14.77033138771988
| Epoch (UTC): | 31 May 2023 04:31:51 |
| Eccentricity: | 0.0007390 |
| inclination: | 98.1752° |
| perigee height: | 633 km |
| apogee height: | 644 km |
| right ascension of ascending node: | 43.2876° |
| argument of perigee: | 285.1659° |
| revolutions per day: | 14.77033138 |
| mean anomaly at epoch: | 74.8733° |
| orbit number at epoch: | 77198 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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