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 40071U 14037C 24277.21221723 .00007337 00000-0 84826-3 0 9990
2 40071 98.3282 194.6339 0009044 124.8948 235.3117 14.85852052553672
Epoch (UTC): | 03 October 2024 05:05:35 |
Eccentricity: | 0.0009044 |
inclination: | 98.3282° |
perigee height: | 604 km |
apogee height: | 617 km |
right ascension of ascending node: | 194.6339° |
argument of perigee: | 124.8948° |
revolutions per day: | 14.85852052 |
mean anomaly at epoch: | 235.3117° |
orbit number at epoch: | 55367 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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