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 15890U 85058B 24357.69738204 .00000835 00000-0 94557-4 0 9999
2 15890 82.5251 210.0048 0020564 160.0304 200.1722 14.85115829110846
| Epoch (UTC): | 22 December 2024 16:44:13 |
| Eccentricity: | 0.0020564 |
| inclination: | 82.5251° |
| perigee height: | 599 km |
| apogee height: | 627 km |
| right ascension of ascending node: | 210.0048° |
| argument of perigee: | 160.0304° |
| revolutions per day: | 14.85115829 |
| mean anomaly at epoch: | 200.1722° |
| orbit number at epoch: | 11084 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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