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 14700U 84013B 23150.49470203 .00000454 00000-0 51713-4 0 9992
2 14700 82.5358 285.9692 0019585 6.1010 62.5361 14.83830119102084
Epoch (UTC): | 30 May 2023 11:52:22 |
Eccentricity: | 0.0019585 |
inclination: | 82.5358° |
perigee height: | 603 km |
apogee height: | 631 km |
right ascension of ascending node: | 285.9692° |
argument of perigee: | 6.1010° |
revolutions per day: | 14.83830119 |
mean anomaly at epoch: | 62.5361° |
orbit number at epoch: | 10208 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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