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 24263.54709119 .00001525 00000-0 13119-2 0 9994
2 00082 38.8521 199.6597 1165163 30.2787 336.0301 12.27031698998703
| Epoch (UTC): | 19 September 2024 13:07:48 |
| Eccentricity: | 0.1165163 |
| inclination: | 38.8521° |
| perigee height: | 637 km |
| apogee height: | 2487 km |
| right ascension of ascending node: | 199.6597° |
| argument of perigee: | 30.2787° |
| revolutions per day: | 12.27031698 |
| mean anomaly at epoch: | 336.0301° |
| orbit number at epoch: | 99870 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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