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 22109U 92058B 24280.91077756 .00006955 00000-0 89280-3 0 9991
2 22109 19.7804 128.3409 0032863 201.7265 158.1753 14.77481742703800
| Epoch (UTC): | 06 October 2024 21:51:31 |
| Eccentricity: | 0.0032863 |
| inclination: | 19.7804° |
| perigee height: | 614 km |
| apogee height: | 660 km |
| right ascension of ascending node: | 128.3409° |
| argument of perigee: | 201.7265° |
| revolutions per day: | 14.77481742 |
| mean anomaly at epoch: | 158.1753° |
| orbit number at epoch: | 70380 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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