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 28415U 04035C 25196.83760230 .00005600 00000-0 22615-3 0 9994
2 28415 97.3779 229.3181 0037370 86.7726 273.7786 15.24518499143776
| Epoch (UTC): | 15 July 2025 20:06:08 |
| Eccentricity: | 0.0037370 |
| inclination: | 97.3779° |
| perigee height: | 466 km |
| apogee height: | 518 km |
| right ascension of ascending node: | 229.3181° |
| argument of perigee: | 86.7726° |
| revolutions per day: | 15.24518499 |
| mean anomaly at epoch: | 273.7786° |
| orbit number at epoch: | 14377 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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