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 15752U 85041B 24357.74775051 .00000104 00000-0 95873-4 0 9996
2 15752 82.9502 81.1730 0025033 56.4219 303.9321 13.73280516982408
| Epoch (UTC): | 22 December 2024 17:56:45 |
| Eccentricity: | 0.0025033 |
| inclination: | 82.9502° |
| perigee height: | 969 km |
| apogee height: | 1006 km |
| right ascension of ascending node: | 81.1730° |
| argument of perigee: | 56.4219° |
| revolutions per day: | 13.73280516 |
| mean anomaly at epoch: | 303.9321° |
| orbit number at epoch: | 98240 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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