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 22231.51596949 .00004894 00000-0 92935-4 0 9995
2 25544 51.6438 22.8500 0005540 138.1257 333.3014 15.50229939355002
| Epoch (UTC): | 19 August 2022 12:22:59 |
| Eccentricity: | 0.0005540 |
| inclination: | 51.6438° |
| perigee height: | 412 km |
| apogee height: | 420 km |
| right ascension of ascending node: | 22.8500° |
| argument of perigee: | 138.1257° |
| revolutions per day: | 15.50229939 |
| mean anomaly at epoch: | 333.3014° |
| orbit number at epoch: | 35500 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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