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 01430U 65051A 23082.33056709 .00000385 00000-0 13194-3 0 9990
2 01430 98.3931 199.3166 0056729 30.6634 329.7850 14.40545871 25694
Epoch (UTC): | 23 March 2023 07:56:00 |
Eccentricity: | 0.0056729 |
inclination: | 98.3931° |
perigee height: | 716 km |
apogee height: | 797 km |
right ascension of ascending node: | 199.3166° |
argument of perigee: | 30.6634° |
revolutions per day: | 14.40545871 |
mean anomaly at epoch: | 329.7850° |
orbit number at epoch: | 2569 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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