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 00029U 60002B 23271.60550118 .00001330 00000-0 22249-3 0 9999
2 00029 48.3796 51.2567 0023891 320.3464 39.5701 14.75565104395371
Epoch (UTC): | 28 September 2023 14:31:55 |
Eccentricity: | 0.0023891 |
inclination: | 48.3796° |
perigee height: | 626 km |
apogee height: | 660 km |
right ascension of ascending node: | 51.2567° |
argument of perigee: | 320.3464° |
revolutions per day: | 14.75565104 |
mean anomaly at epoch: | 39.5701° |
orbit number at epoch: | 39537 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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