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 18509U 82051E 24262.79417317 .00004734 00000-0 10374-2 0 9999
2 18509 74.0034 128.0907 0007782 291.5222 187.4933 14.57917404984779
Epoch (UTC): | 18 September 2024 19:03:36 |
Eccentricity: | 0.0007782 |
inclination: | 74.0034° |
perigee height: | 694 km |
apogee height: | 705 km |
right ascension of ascending node: | 128.0907° |
argument of perigee: | 291.5222° |
revolutions per day: | 14.57917404 |
mean anomaly at epoch: | 187.4933° |
orbit number at epoch: | 98477 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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