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 53483C 22099U 24281.13937500 -.00033514 00000+0 -26142-2 0 2818
2 53483 97.6553 40.3994 0001753 89.7854 292.9196 15.01296085 12
| Epoch (UTC): | 07 October 2024 03:20:42 |
| Eccentricity: | 0.0001753 |
| inclination: | 97.6553° |
| perigee height: | 561 km |
| apogee height: | 564 km |
| right ascension of ascending node: | 40.3994° |
| argument of perigee: | 89.7854° |
| revolutions per day: | 15.01296085 |
| mean anomaly at epoch: | 292.9196° |
| orbit number at epoch: | 1 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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