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 23151.69872672 .00018492 00000-0 32716-3 0 9995
2 25544 51.6407 50.2755 0005629 38.0975 48.7506 15.50341747399236
| Epoch (UTC): | 31 May 2023 16:46:09 |
| Eccentricity: | 0.0005629 |
| inclination: | 51.6407° |
| perigee height: | 412 km |
| apogee height: | 419 km |
| right ascension of ascending node: | 50.2755° |
| argument of perigee: | 38.0975° |
| revolutions per day: | 15.50341747 |
| mean anomaly at epoch: | 48.7506° |
| orbit number at epoch: | 39923 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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