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 43784U 18099AC 25138.71904220 .00011045 00000-0 55920-3 0 9992
2 43784 97.4421 193.4969 0002848 202.5207 157.5902 15.17165651353329
| Epoch (UTC): | 18 May 2025 17:15:25 |
| Eccentricity: | 0.0002848 |
| inclination: | 97.4421° |
| perigee height: | 512 km |
| apogee height: | 516 km |
| right ascension of ascending node: | 193.4969° |
| argument of perigee: | 202.5207° |
| revolutions per day: | 15.17165651 |
| mean anomaly at epoch: | 157.5902° |
| orbit number at epoch: | 35332 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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