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 26932U 01043D 25196.60121200 -.00000003 00000-0 30213-4 0 9992
2 26932 67.0559 42.4258 0004364 273.7686 86.2916 14.31149981242222
| Epoch (UTC): | 15 July 2025 14:25:44 |
| Eccentricity: | 0.0004364 |
| inclination: | 67.0559° |
| perigee height: | 785 km |
| apogee height: | 791 km |
| right ascension of ascending node: | 42.4258° |
| argument of perigee: | 273.7686° |
| revolutions per day: | 14.31149981 |
| mean anomaly at epoch: | 86.2916° |
| orbit number at epoch: | 24222 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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