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 19274U 88056A 25189.40894164 .00005371 00000-0 20623-3 0 9993
2 19274 82.4725 149.9892 0012778 323.9283 36.1092 15.26159237997759
| Epoch (UTC): | 08 July 2025 09:48:52 |
| Eccentricity: | 0.0012778 |
| inclination: | 82.4725° |
| perigee height: | 478 km |
| apogee height: | 496 km |
| right ascension of ascending node: | 149.9892° |
| argument of perigee: | 323.9283° |
| revolutions per day: | 15.26159237 |
| mean anomaly at epoch: | 36.1092° |
| orbit number at epoch: | 99775 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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