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 45119U 19071J 23100.59666950 .12876049 12467-4 44960-3 0 9997
2 45119 51.6129 8.2149 0006761 246.9747 113.0568 16.44056360179702
| Epoch (UTC): | 10 April 2023 14:19:12 |
| Eccentricity: | 0.0006761 |
| inclination: | 51.6129° |
| perigee height: | 150 km |
| apogee height: | 159 km |
| right ascension of ascending node: | 8.2149° |
| argument of perigee: | 246.9747° |
| revolutions per day: | 16.44056360 |
| mean anomaly at epoch: | 113.0568° |
| orbit number at epoch: | 17970 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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