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 03598U 68110B 23333.47666093 .00001643 00000-0 37072-3 0 9992
2 03598 34.9947 345.7760 0048943 269.1846 90.3239 14.55474851888845
| Epoch (UTC): | 29 November 2023 11:26:23 |
| Eccentricity: | 0.0048943 |
| inclination: | 34.9947° |
| perigee height: | 673 km |
| apogee height: | 742 km |
| right ascension of ascending node: | 345.7760° |
| argument of perigee: | 269.1846° |
| revolutions per day: | 14.55474851 |
| mean anomaly at epoch: | 90.3239° |
| orbit number at epoch: | 88884 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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