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 877U 64053B 25200.51496469 .00000095 00000-0 43037-4 0 9998
2 877 65.0779 294.6807 0057960 14.7095 345.5674 14.61105328232728
| Epoch (UTC): | 19 July 2025 12:21:32 |
| Eccentricity: | 0.0057960 |
| inclination: | 65.0779° |
| perigee height: | 648 km |
| apogee height: | 730 km |
| right ascension of ascending node: | 294.6807° |
| argument of perigee: | 14.7095° |
| revolutions per day: | 14.61105328 |
| mean anomaly at epoch: | 345.5674° |
| orbit number at epoch: | 23272 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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