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 32787U 08021E 23080.89330988 .00013651 00000-0 11131-2 0 9994
2 32787 97.5975 59.3935 0008218 309.4855 50.5641 14.99551646809613
| Epoch (UTC): | 21 March 2023 21:26:21 |
| Eccentricity: | 0.0008218 |
| inclination: | 97.5975° |
| perigee height: | 562 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 59.3935° |
| argument of perigee: | 309.4855° |
| revolutions per day: | 14.99551646 |
| mean anomaly at epoch: | 50.5641° |
| orbit number at epoch: | 80961 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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