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 33591U 09005A 22024.77027039 .00000034 00000-0 43647-4 0 9995
2 33591 99.1660 55.7640 0013255 229.1039 130.8984 14.12524380668163
| Epoch (UTC): | 24 January 2022 18:29:11 |
| Eccentricity: | 0.0013255 |
| inclination: | 99.1660° |
| perigee height: | 841 km |
| apogee height: | 860 km |
| right ascension of ascending node: | 55.7640° |
| argument of perigee: | 229.1039° |
| revolutions per day: | 14.12524380 |
| mean anomaly at epoch: | 130.8984° |
| orbit number at epoch: | 66816 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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