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 22147.88175692 -.00000020 00000-0 95741-5 0 9997
2 00082 38.8633 91.5585 1173488 267.2518 79.3595 12.26015591894886
| Epoch (UTC): | 27 May 2022 21:09:43 |
| Eccentricity: | 0.1173488 |
| inclination: | 38.8633° |
| perigee height: | 634 km |
| apogee height: | 2499 km |
| right ascension of ascending node: | 91.5585° |
| argument of perigee: | 267.2518° |
| revolutions per day: | 12.26015591 |
| mean anomaly at epoch: | 79.3595° |
| orbit number at epoch: | 89488 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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