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 22018.82648066 -.00000001 00000-0 43856-4 0 9996
2 00082 38.8534 209.3768 1174221 4.4539 356.5609 12.26009713879044
| Epoch (UTC): | 18 January 2022 19:50:07 |
| Eccentricity: | 0.1174221 |
| inclination: | 38.8534° |
| perigee height: | 633 km |
| apogee height: | 2499 km |
| right ascension of ascending node: | 209.3768° |
| argument of perigee: | 4.4539° |
| revolutions per day: | 12.26009713 |
| mean anomaly at epoch: | 356.5609° |
| orbit number at epoch: | 87904 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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