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 25544U 98067A 22334.92807094 .00090592 00000-0 15956-2 0 9996
2 25544 51.6426 230.5638 0004839 117.4083 329.1930 15.49661159371040
| Epoch (UTC): | 30 November 2022 22:16:25 |
| Eccentricity: | 0.0004839 |
| inclination: | 51.6426° |
| perigee height: | 414 km |
| apogee height: | 421 km |
| right ascension of ascending node: | 230.5638° |
| argument of perigee: | 117.4083° |
| revolutions per day: | 15.49661159 |
| mean anomaly at epoch: | 329.1930° |
| orbit number at epoch: | 37104 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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