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 23081.46706451 .00015459 00000-0 11886-2 0 9996
2 32788 97.5577 62.9733 0004223 296.1367 63.9423 15.01791251810182
Epoch (UTC): | 22 March 2023 11:12:34 |
Eccentricity: | 0.0004223 |
inclination: | 97.5577° |
perigee height: | 558 km |
apogee height: | 564 km |
right ascension of ascending node: | 62.9733° |
argument of perigee: | 296.1367° |
revolutions per day: | 15.01791251 |
mean anomaly at epoch: | 63.9423° |
orbit number at epoch: | 81018 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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