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 22269.45326302 .00001335 00000-0 18275-3 0 9992
2 33498 98.1545 163.1106 0009359 290.0128 70.0075 14.80219092736378
| Epoch (UTC): | 26 September 2022 10:52:41 |
| Eccentricity: | 0.0009359 |
| inclination: | 98.1545° |
| perigee height: | 622 km |
| apogee height: | 635 km |
| right ascension of ascending node: | 163.1106° |
| argument of perigee: | 290.0128° |
| revolutions per day: | 14.80219092 |
| mean anomaly at epoch: | 70.0075° |
| orbit number at epoch: | 73637 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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