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 32788U 08021F 22176.52263629 .00002840 00000-0 24776-3 0 9995
2 32788 97.5339 161.5517 0013426 93.9633 266.3124 14.97549372769749
Epoch (UTC): | 25 June 2022 12:32:35 |
Eccentricity: | 0.0013426 |
inclination: | 97.5339° |
perigee height: | 565 km |
apogee height: | 584 km |
right ascension of ascending node: | 161.5517° |
argument of perigee: | 93.9633° |
revolutions per day: | 14.97549372 |
mean anomaly at epoch: | 266.3124° |
orbit number at epoch: | 76974 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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