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 22178.76137150 .00000127 00000-0 93633-4 0 9993
2 33591 99.1468 213.1145 0014393 155.4357 204.7503 14.12581492689907
| Epoch (UTC): | 27 June 2022 18:16:22 |
| Eccentricity: | 0.0014393 |
| inclination: | 99.1468° |
| perigee height: | 840 km |
| apogee height: | 861 km |
| right ascension of ascending node: | 213.1145° |
| argument of perigee: | 155.4357° |
| revolutions per day: | 14.12581492 |
| mean anomaly at epoch: | 204.7503° |
| orbit number at epoch: | 68990 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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