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 25544U 98067A 25109.51643189 .00016574 00000-0 30074-3 0 9994
2 25544 51.6360 237.6338 0005358 55.3016 304.8477 15.49708747506068
| Epoch (UTC): | 19 April 2025 12:23:39 |
| Eccentricity: | 0.0005358 |
| inclination: | 51.6360° |
| perigee height: | 414 km |
| apogee height: | 421 km |
| right ascension of ascending node: | 237.6338° |
| argument of perigee: | 55.3016° |
| revolutions per day: | 15.49708747 |
| mean anomaly at epoch: | 304.8477° |
| orbit number at epoch: | 50606 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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