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 37227U 10062F 23088.52684180 .00002831 00000-0 37452-3 0 9993
2 37227 71.9682 235.0512 0015446 170.8438 189.3011 14.80676804191575
Epoch (UTC): | 29 March 2023 12:38:39 |
Eccentricity: | 0.0015446 |
inclination: | 71.9682° |
perigee height: | 616 km |
apogee height: | 638 km |
right ascension of ascending node: | 235.0512° |
argument of perigee: | 170.8438° |
revolutions per day: | 14.80676804 |
mean anomaly at epoch: | 189.3011° |
orbit number at epoch: | 19157 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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