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 44607U 16068G 24355.23993266 .00001602 00000-0 10071-2 0 9991
2 44607 98.4484 159.7240 0205192 248.3673 109.5523 13.95876942404917
| Epoch (UTC): | 20 December 2024 05:45:30 |
| Eccentricity: | 0.0205192 |
| inclination: | 98.4484° |
| perigee height: | 758 km |
| apogee height: | 1057 km |
| right ascension of ascending node: | 159.7240° |
| argument of perigee: | 248.3673° |
| revolutions per day: | 13.95876942 |
| mean anomaly at epoch: | 109.5523° |
| orbit number at epoch: | 40491 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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