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 45117U 19071G 22177.10640847 .00028232 00000-0 52647-3 0 9999
2 45117 51.6373 11.6710 0008555 200.6796 159.3847 15.48543994134775
| Epoch (UTC): | 26 June 2022 02:33:13 |
| Eccentricity: | 0.0008555 |
| inclination: | 51.6373° |
| perigee height: | 415 km |
| apogee height: | 427 km |
| right ascension of ascending node: | 11.6710° |
| argument of perigee: | 200.6796° |
| revolutions per day: | 15.48543994 |
| mean anomaly at epoch: | 159.3847° |
| orbit number at epoch: | 13477 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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