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 23156.91196170 .00000009 00000-0 -65923-5 0 9998
2 14974 82.9341 320.6259 0045535 22.8153 86.7109 13.76980405961925
| Epoch (UTC): | 05 June 2023 21:53:13 |
| Eccentricity: | 0.0045535 |
| inclination: | 82.9341° |
| perigee height: | 941 km |
| apogee height: | 1008 km |
| right ascension of ascending node: | 320.6259° |
| argument of perigee: | 22.8153° |
| revolutions per day: | 13.76980405 |
| mean anomaly at epoch: | 86.7109° |
| orbit number at epoch: | 96192 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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