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 30903U 99025AYR 24352.43875942 .00000652 00000-0 47895-3 0 9997
2 30903 99.4186 223.9598 0096503 353.1496 6.8341 13.97355821636726
Epoch (UTC): | 17 December 2024 10:31:48 |
Eccentricity: | 0.0096503 |
inclination: | 99.4186° |
perigee height: | 833 km |
apogee height: | 973 km |
right ascension of ascending node: | 223.9598° |
argument of perigee: | 353.1496° |
revolutions per day: | 13.97355821 |
mean anomaly at epoch: | 6.8341° |
orbit number at epoch: | 63672 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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