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 22U 59009A 23333.16667784 .00013251 00000-0 83878-3 0 9995
2 22 50.2802 291.1271 0121380 48.7364 312.3966 15.03307407414080
| Epoch (UTC): | 29 November 2023 04:00:00 |
| Eccentricity: | 0.0121380 |
| inclination: | 50.2802° |
| perigee height: | 472 km |
| apogee height: | 641 km |
| right ascension of ascending node: | 291.1271° |
| argument of perigee: | 48.7364° |
| revolutions per day: | 15.03307407 |
| mean anomaly at epoch: | 312.3966° |
| orbit number at epoch: | 41408 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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