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 23343.07755144 .00026603 00000-0 46764-3 0 9995
2 25544 51.6400 182.2887 0001365 15.2823 127.3497 15.50296263428916
| Epoch (UTC): | 09 December 2023 01:51:40 |
| Eccentricity: | 0.0001365 |
| inclination: | 51.6400° |
| perigee height: | 415 km |
| apogee height: | 417 km |
| right ascension of ascending node: | 182.2887° |
| argument of perigee: | 15.2823° |
| revolutions per day: | 15.50296263 |
| mean anomaly at epoch: | 127.3497° |
| orbit number at epoch: | 42891 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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