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 24256.96297258 .00050034 00000-0 29639-2 0 9998
2 40021 98.0974 245.5506 0014108 150.9212 209.2804 15.11132227557363
Epoch (UTC): | 12 September 2024 23:06:40 |
Eccentricity: | 0.0014108 |
inclination: | 98.0974° |
perigee height: | 523 km |
apogee height: | 542 km |
right ascension of ascending node: | 245.5506° |
argument of perigee: | 150.9212° |
revolutions per day: | 15.11132227 |
mean anomaly at epoch: | 209.2804° |
orbit number at epoch: | 55736 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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