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 22176.92354035 .00003024 00000-0 26345-3 0 9990
2 32788 97.5339 161.9385 0013388 92.7507 267.5248 14.97552605769709
| Epoch (UTC): | 25 June 2022 22:09:53 |
| Eccentricity: | 0.0013388 |
| inclination: | 97.5339° |
| perigee height: | 565 km |
| apogee height: | 584 km |
| right ascension of ascending node: | 161.9385° |
| argument of perigee: | 92.7507° |
| revolutions per day: | 14.97552605 |
| mean anomaly at epoch: | 267.5248° |
| orbit number at epoch: | 76970 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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