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 23151.59900733 -.00000015 00000-0 -31062-4 0 9999
2 14974 82.9341 324.5803 0045846 37.4535 29.9390 13.76980409961198
| Epoch (UTC): | 31 May 2023 14:22:34 |
| Eccentricity: | 0.0045846 |
| inclination: | 82.9341° |
| perigee height: | 941 km |
| apogee height: | 1008 km |
| right ascension of ascending node: | 324.5803° |
| argument of perigee: | 37.4535° |
| revolutions per day: | 13.76980409 |
| mean anomaly at epoch: | 29.9390° |
| orbit number at epoch: | 96119 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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