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 22279.79366618 .00000197 00000-0 19505-3 0 9999
2 00082 38.8571 323.2160 1169967 183.8299 175.2723 12.26028014911071
| Epoch (UTC): | 06 October 2022 19:02:52 |
| Eccentricity: | 0.1169967 |
| inclination: | 38.8571° |
| perigee height: | 637 km |
| apogee height: | 2496 km |
| right ascension of ascending node: | 323.2160° |
| argument of perigee: | 183.8299° |
| revolutions per day: | 12.26028014 |
| mean anomaly at epoch: | 175.2723° |
| orbit number at epoch: | 91107 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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