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 36092U 09061E 24278.91419618 .00027437 00000-0 83652-2 0 9997
2 36092 98.7281 262.1623 0134383 45.2385 15.8765 14.36776228776051
| Epoch (UTC): | 04 October 2024 21:56:26 |
| Eccentricity: | 0.0134383 |
| inclination: | 98.7281° |
| perigee height: | 673 km |
| apogee height: | 865 km |
| right ascension of ascending node: | 262.1623° |
| argument of perigee: | 45.2385° |
| revolutions per day: | 14.36776228 |
| mean anomaly at epoch: | 15.8765° |
| orbit number at epoch: | 77605 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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