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 42640U 75052LZ 24274.45616911 .00001538 00000-0 23561-2 0 9993
2 42640 99.7719 88.4002 0217687 162.2437 228.7183 13.44303858532075
Epoch (UTC): | 30 September 2024 10:56:53 |
Eccentricity: | 0.0217687 |
inclination: | 99.7719° |
perigee height: | 930 km |
apogee height: | 1256 km |
right ascension of ascending node: | 88.4002° |
argument of perigee: | 162.2437° |
revolutions per day: | 13.44303858 |
mean anomaly at epoch: | 228.7183° |
orbit number at epoch: | 53207 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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