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 23345.51867810 .00009795 00000-0 17731-3 0 9995
2 25544 51.6401 170.1832 0001017 37.0320 58.7854 15.50331619429292
| Epoch (UTC): | 11 December 2023 12:26:53 |
| Eccentricity: | 0.0001017 |
| inclination: | 51.6401° |
| perigee height: | 415 km |
| apogee height: | 416 km |
| right ascension of ascending node: | 170.1832° |
| argument of perigee: | 37.0320° |
| revolutions per day: | 15.50331619 |
| mean anomaly at epoch: | 58.7854° |
| orbit number at epoch: | 42929 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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