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 00022U 59009A 23336.29082499 .00025668 00000-0 15996-2 0 9996
2 00022 50.2795 276.2813 0121110 60.8915 300.4098 15.03409150659594
| Epoch (UTC): | 02 December 2023 06:58:47 |
| Eccentricity: | 0.0121110 |
| inclination: | 50.2795° |
| perigee height: | 472 km |
| apogee height: | 640 km |
| right ascension of ascending node: | 276.2813° |
| argument of perigee: | 60.8915° |
| revolutions per day: | 15.03409150 |
| mean anomaly at epoch: | 300.4098° |
| orbit number at epoch: | 65959 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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