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 23152.83455441 .00000505 00000-0 27267-3 0 9999
2 25733 98.8211 195.8147 0015994 124.9308 235.3372 14.17042952242515
Epoch (UTC): | 01 June 2023 20:01:45 |
Eccentricity: | 0.0015994 |
inclination: | 98.8211° |
perigee height: | 824 km |
apogee height: | 847 km |
right ascension of ascending node: | 195.8147° |
argument of perigee: | 124.9308° |
revolutions per day: | 14.17042952 |
mean anomaly at epoch: | 235.3372° |
orbit number at epoch: | 24251 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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