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 14506U 83113A 23156.52951703 .00000279 00000-0 12787-3 0 9997
2 14506 98.2979 331.6610 0009806 262.9568 165.6126 14.28518346 57273
Epoch (UTC): | 05 June 2023 12:42:30 |
Eccentricity: | 0.0009806 |
inclination: | 98.2979° |
perigee height: | 789 km |
apogee height: | 804 km |
right ascension of ascending node: | 331.6610° |
argument of perigee: | 262.9568° |
revolutions per day: | 14.28518346 |
mean anomaly at epoch: | 165.6126° |
orbit number at epoch: | 5727 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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