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 31257U 99025BMP 22176.07177469 .00001799 00000-0 10801-2 0 9990
2 31257 98.7428 287.2458 0130174 74.0807 287.4661 14.03966380778484
Epoch (UTC): | 25 June 2022 01:43:21 |
Eccentricity: | 0.0130174 |
inclination: | 98.7428° |
perigee height: | 785 km |
apogee height: | 974 km |
right ascension of ascending node: | 287.2458° |
argument of perigee: | 74.0807° |
revolutions per day: | 14.03966380 |
mean anomaly at epoch: | 287.4661° |
orbit number at epoch: | 77848 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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