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 33498U 09002G 23150.52120053 .00002196 00000-0 28405-3 0 9997
2 33498 98.1380 53.0922 0009474 203.6699 156.4078 14.81930261772796
| Epoch (UTC): | 30 May 2023 12:30:31 |
| Eccentricity: | 0.0009474 |
| inclination: | 98.1380° |
| perigee height: | 616 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 53.0922° |
| argument of perigee: | 203.6699° |
| revolutions per day: | 14.81930261 |
| mean anomaly at epoch: | 156.4078° |
| orbit number at epoch: | 77279 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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