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 30475U 99025AGN 24337.93616150 .00003303 00000-0 17437-2 0 9997
2 30475 98.8119 18.6498 0043631 278.8713 204.3367 14.14060315916518
Epoch (UTC): | 02 December 2024 22:28:04 |
Eccentricity: | 0.0043631 |
inclination: | 98.8119° |
perigee height: | 814 km |
apogee height: | 877 km |
right ascension of ascending node: | 18.6498° |
argument of perigee: | 278.8713° |
revolutions per day: | 14.14060315 |
mean anomaly at epoch: | 204.3367° |
orbit number at epoch: | 91651 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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