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 3230U 68040B 24277.19143179 .00009753 00000-0 82856-3 0 9999
2 3230 74.0325 297.3166 0028234 260.9570 98.8420 14.97665720 32860
Epoch (UTC): | 03 October 2024 04:35:39 |
Eccentricity: | 0.0028234 |
inclination: | 74.0325° |
perigee height: | 554 km |
apogee height: | 594 km |
right ascension of ascending node: | 297.3166° |
argument of perigee: | 260.9570° |
revolutions per day: | 14.97665720 |
mean anomaly at epoch: | 98.8420° |
orbit number at epoch: | 3286 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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