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 53499C 22099AL 24280.14076389 -.00002276 00000+0 -17754-3 0 2804
2 53499 97.6559 39.3787 0001734 98.5320 330.4947 15.01256068 17
| Epoch (UTC): | 06 October 2024 03:22:42 |
| Eccentricity: | 0.0001734 |
| inclination: | 97.6559° |
| perigee height: | 562 km |
| apogee height: | 564 km |
| right ascension of ascending node: | 39.3787° |
| argument of perigee: | 98.5320° |
| revolutions per day: | 15.01256068 |
| mean anomaly at epoch: | 330.4947° |
| 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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