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 44609U 17060B 24358.03392341 .00011327 00000-0 10909-2 0 9999
2 44609 97.5813 23.5707 0035608 330.5007 29.4203 14.92622982384226
| Epoch (UTC): | 23 December 2024 00:48:50 |
| Eccentricity: | 0.0035608 |
| inclination: | 97.5813° |
| perigee height: | 565 km |
| apogee height: | 614 km |
| right ascension of ascending node: | 23.5707° |
| argument of perigee: | 330.5007° |
| revolutions per day: | 14.92622982 |
| mean anomaly at epoch: | 29.4203° |
| orbit number at epoch: | 38422 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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