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 14974U 84046B 23151.02762363 -.00000013 00000-0 -28478-4 0 9997
2 14974 82.9341 325.0056 0045875 39.0259 77.5428 13.76980462961344
Epoch (UTC): | 31 May 2023 00:39:46 |
Eccentricity: | 0.0045875 |
inclination: | 82.9341° |
perigee height: | 941 km |
apogee height: | 1008 km |
right ascension of ascending node: | 325.0056° |
argument of perigee: | 39.0259° |
revolutions per day: | 13.76980462 |
mean anomaly at epoch: | 77.5428° |
orbit number at epoch: | 96134 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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