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 00051U 60009C 25193.88009291 -.00000088 00000-0 -43166-4 0 9990
2 00051 47.2151 19.2893 0106616 267.6237 91.2342 12.18362577889809
| Epoch (UTC): | 12 July 2025 21:07:20 |
| Eccentricity: | 0.0106616 |
| inclination: | 47.2151° |
| perigee height: | 1514 km |
| apogee height: | 1685 km |
| right ascension of ascending node: | 19.2893° |
| argument of perigee: | 267.6237° |
| revolutions per day: | 12.18362577 |
| mean anomaly at epoch: | 91.2342° |
| orbit number at epoch: | 88980 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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