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 36798U 10035D 25322.48189073 .00001319 00000-0 20767-3 0 9995
2 36798 97.7637 328.8512 0001464 108.5406 251.5962 14.74054423822716
| Epoch (UTC): | 18 November 2025 11:33:55 |
| Eccentricity: | 0.0001464 |
| inclination: | 97.7637° |
| perigee height: | 647 km |
| apogee height: | 649 km |
| right ascension of ascending node: | 328.8512° |
| argument of perigee: | 108.5406° |
| revolutions per day: | 14.74054423 |
| mean anomaly at epoch: | 251.5962° |
| orbit number at epoch: | 82271 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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