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 25733U 99025D 23150.08079612 .00000461 00000-0 25078-3 0 9995
2 25733 98.8213 193.0826 0015914 132.2863 227.9663 14.17039677242128
Epoch (UTC): | 30 May 2023 01:56:20 |
Eccentricity: | 0.0015914 |
inclination: | 98.8213° |
perigee height: | 824 km |
apogee height: | 847 km |
right ascension of ascending node: | 193.0826° |
argument of perigee: | 132.2863° |
revolutions per day: | 14.17039677 |
mean anomaly at epoch: | 227.9663° |
orbit number at epoch: | 24212 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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