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 14085U 83048B 23154.41685547 .00000098 00000-0 84062-4 0 9997
2 14085 82.9434 273.6153 0034579 135.7279 224.6653 13.76393690 9878
| Epoch (UTC): | 03 June 2023 10:00:16 |
| Eccentricity: | 0.0034579 |
| inclination: | 82.9434° |
| perigee height: | 951 km |
| apogee height: | 1002 km |
| right ascension of ascending node: | 273.6153° |
| argument of perigee: | 135.7279° |
| revolutions per day: | 13.76393690 |
| mean anomaly at epoch: | 224.6653° |
| orbit number at epoch: | 987 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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