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 58315U 23174BM 24315.17596867 .00030217 00000-0 11832-2 0 9993
2 58315 97.4379 28.3878 0009995 71.2625 288.9697 15.25706089 55927
Epoch (UTC): | 10 November 2024 04:13:23 |
Eccentricity: | 0.0009995 |
inclination: | 97.4379° |
perigee height: | 482 km |
apogee height: | 495 km |
right ascension of ascending node: | 28.3878° |
argument of perigee: | 71.2625° |
revolutions per day: | 15.25706089 |
mean anomaly at epoch: | 288.9697° |
orbit number at epoch: | 5592 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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