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 22137.21697095 .00002050 00000-0 27879-3 0 9995
2 33498 98.1726 28.6849 0010790 0.6621 359.4602 14.79894489717233
| Epoch (UTC): | 17 May 2022 05:12:26 |
| Eccentricity: | 0.0010790 |
| inclination: | 98.1726° |
| perigee height: | 622 km |
| apogee height: | 637 km |
| right ascension of ascending node: | 28.6849° |
| argument of perigee: | 0.6621° |
| revolutions per day: | 14.79894489 |
| mean anomaly at epoch: | 359.4602° |
| orbit number at epoch: | 71723 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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