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 15751U 85041A 23088.82397590 .00000128 00000-0 12379-3 0 9997
2 15751 82.9516 211.8877 0027974 117.6872 354.1700 13.71767494893545
| Epoch (UTC): | 29 March 2023 19:46:31 |
| Eccentricity: | 0.0027974 |
| inclination: | 82.9516° |
| perigee height: | 972 km |
| apogee height: | 1014 km |
| right ascension of ascending node: | 211.8877° |
| argument of perigee: | 117.6872° |
| revolutions per day: | 13.71767494 |
| mean anomaly at epoch: | 354.1700° |
| orbit number at epoch: | 89354 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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