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 22146.57814721 .00000002 00000-0 26987-4 0 9999
2 00082 38.8629 96.3836 1173486 260.9685 85.6661 12.26015529894724
| Epoch (UTC): | 26 May 2022 13:52:31 |
| Eccentricity: | 0.1173486 |
| inclination: | 38.8629° |
| perigee height: | 634 km |
| apogee height: | 2499 km |
| right ascension of ascending node: | 96.3836° |
| argument of perigee: | 260.9685° |
| revolutions per day: | 12.26015529 |
| mean anomaly at epoch: | 85.6661° |
| orbit number at epoch: | 89472 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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