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 12U 59001B 24306.28470474 .00002706 00000-0 15666-2 0 9990
2 12 32.9011 152.8610 1652250 208.1156 141.9617 11.47338156705750
Epoch (UTC): | 01 November 2024 06:49:58 |
Eccentricity: | 0.1652250 |
inclination: | 32.9011° |
perigee height: | 553 km |
apogee height: | 3297 km |
right ascension of ascending node: | 152.8610° |
argument of perigee: | 208.1156° |
revolutions per day: | 11.47338156 |
mean anomaly at epoch: | 141.9617° |
orbit number at epoch: | 70575 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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