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 25544U 98067A 23335.21280888 .00059007 00000-0 10330-2 0 9993
2 25544 51.6421 221.2609 0001021 355.9322 147.6364 15.50032099427699
Epoch (UTC): | 01 December 2023 05:06:26 |
Eccentricity: | 0.0001021 |
inclination: | 51.6421° |
perigee height: | 416 km |
apogee height: | 417 km |
right ascension of ascending node: | 221.2609° |
argument of perigee: | 355.9322° |
revolutions per day: | 15.50032099 |
mean anomaly at epoch: | 147.6364° |
orbit number at epoch: | 42769 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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