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 23340.44730195 .00009380 00000-0 72609-3 0 9990
2 40021 98.0758 310.5257 0015451 44.7211 315.5255 15.01596604515008
Epoch (UTC): | 06 December 2023 10:44:06 |
Eccentricity: | 0.0015451 |
inclination: | 98.0758° |
perigee height: | 551 km |
apogee height: | 573 km |
right ascension of ascending node: | 310.5257° |
argument of perigee: | 44.7211° |
revolutions per day: | 15.01596604 |
mean anomaly at epoch: | 315.5255° |
orbit number at epoch: | 51500 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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