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 43189U 18014K 24260.72683009 .00011384 00000-0 77764-3 0 9999
2 43189 97.5831 161.0395 0014385 51.1273 309.1235 15.06245720360829
Epoch (UTC): | 16 September 2024 17:26:38 |
Eccentricity: | 0.0014385 |
inclination: | 97.5831° |
perigee height: | 538 km |
apogee height: | 557 km |
right ascension of ascending node: | 161.0395° |
argument of perigee: | 51.1273° |
revolutions per day: | 15.06245720 |
mean anomaly at epoch: | 309.1235° |
orbit number at epoch: | 36082 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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