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 00082U 61004B 24250.43715123 .00001958 00000-0 16537-2 0 9997
2 00082 38.8565 248.2774 1165834 326.8817 26.3833 12.26982694997092
| Epoch (UTC): | 06 September 2024 10:29:29 |
| Eccentricity: | 0.1165834 |
| inclination: | 38.8565° |
| perigee height: | 636 km |
| apogee height: | 2488 km |
| right ascension of ascending node: | 248.2774° |
| argument of perigee: | 326.8817° |
| revolutions per day: | 12.26982694 |
| mean anomaly at epoch: | 26.3833° |
| orbit number at epoch: | 99709 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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