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 40021U 14033M 24279.93060274 .00047006 00000-0 26787-2 0 9992
2 40021 98.0984 269.8845 0015087 86.7970 273.4985 15.12537037560831
Epoch (UTC): | 05 October 2024 22:20:04 |
Eccentricity: | 0.0015087 |
inclination: | 98.0984° |
perigee height: | 518 km |
apogee height: | 539 km |
right ascension of ascending node: | 269.8845° |
argument of perigee: | 86.7970° |
revolutions per day: | 15.12537037 |
mean anomaly at epoch: | 273.4985° |
orbit number at epoch: | 56083 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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