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 00011U 59001A 24309.25137065 .00002439 00000-0 12644-2 0 9991
2 00011 32.8728 155.6576 1454538 302.9407 43.9423 11.88880026465185
Epoch (UTC): | 04 November 2024 06:01:58 |
Eccentricity: | 0.1454538 |
inclination: | 32.8728° |
perigee height: | 551 km |
apogee height: | 2910 km |
right ascension of ascending node: | 155.6576° |
argument of perigee: | 302.9407° |
revolutions per day: | 11.88880026 |
mean anomaly at epoch: | 43.9423° |
orbit number at epoch: | 46518 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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