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 30349U 99025ABL 24276.18491824 .00011487 00000-0 67593-2 0 9995
2 30349 98.5507 253.8986 0092542 170.9607 320.3448 14.05974209900923
Epoch (UTC): | 02 October 2024 04:26:16 |
Eccentricity: | 0.0092542 |
inclination: | 98.5507° |
perigee height: | 806 km |
apogee height: | 940 km |
right ascension of ascending node: | 253.8986° |
argument of perigee: | 170.9607° |
revolutions per day: | 14.05974209 |
mean anomaly at epoch: | 320.3448° |
orbit number at epoch: | 90092 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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