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 22026.65613466 .00000616 00000-0 89541-4 0 9991
2 33498 98.1869 276.1462 0010797 355.6718 4.4397 14.79580178700887
| Epoch (UTC): | 26 January 2022 15:44:50 |
| Eccentricity: | 0.0010797 |
| inclination: | 98.1869° |
| perigee height: | 623 km |
| apogee height: | 638 km |
| right ascension of ascending node: | 276.1462° |
| argument of perigee: | 355.6718° |
| revolutions per day: | 14.79580178 |
| mean anomaly at epoch: | 4.4397° |
| orbit number at epoch: | 70088 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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