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 07714U 75023A 23156.58408507 .00000166 00000-0 89829-4 0 9993
2 07714 81.2097 229.4458 0028272 232.3364 127.5240 14.08154221791631
Epoch (UTC): | 05 June 2023 14:01:04 |
Eccentricity: | 0.0028272 |
inclination: | 81.2097° |
perigee height: | 845 km |
apogee height: | 886 km |
right ascension of ascending node: | 229.4458° |
argument of perigee: | 232.3364° |
revolutions per day: | 14.08154221 |
mean anomaly at epoch: | 127.5240° |
orbit number at epoch: | 79163 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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