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 23157.07109304 .00000505 00000-0 27245-3 0 9990
2 25733 98.8209 200.0180 0016089 113.7507 246.5357 14.17047722243182
Epoch (UTC): | 06 June 2023 01:42:22 |
Eccentricity: | 0.0016089 |
inclination: | 98.8209° |
perigee height: | 824 km |
apogee height: | 847 km |
right ascension of ascending node: | 200.0180° |
argument of perigee: | 113.7507° |
revolutions per day: | 14.17047722 |
mean anomaly at epoch: | 246.5357° |
orbit number at epoch: | 24318 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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