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 21153U 91019B 25198.42936781 -.00000001 00000-0 -16206-4 0 9999
2 21153 82.9262 166.1696 0028912 179.5309 294.1955 13.76288072724400
| Epoch (UTC): | 17 July 2025 10:18:17 |
| Eccentricity: | 0.0028912 |
| inclination: | 82.9262° |
| perigee height: | 956 km |
| apogee height: | 998 km |
| right ascension of ascending node: | 166.1696° |
| argument of perigee: | 179.5309° |
| revolutions per day: | 13.76288072 |
| mean anomaly at epoch: | 294.1955° |
| orbit number at epoch: | 72440 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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