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 22180.53216094 .00000127 00000-0 93395-4 0 9991
2 33591 99.1467 214.9224 0014481 150.6090 209.5898 14.12582027690156
| Epoch (UTC): | 29 June 2022 12:46:18 |
| Eccentricity: | 0.0014481 |
| inclination: | 99.1467° |
| perigee height: | 840 km |
| apogee height: | 861 km |
| right ascension of ascending node: | 214.9224° |
| argument of perigee: | 150.6090° |
| revolutions per day: | 14.12582027 |
| mean anomaly at epoch: | 209.5898° |
| orbit number at epoch: | 69015 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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