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 13649U 82109B 25198.75863356 .00000201 00000-0 74331-4 0 9996
2 13649 74.0016 327.5432 0017705 153.8711 350.3180 14.38442413235852
| Epoch (UTC): | 17 July 2025 18:12:25 |
| Eccentricity: | 0.0017705 |
| inclination: | 74.0016° |
| perigee height: | 751 km |
| apogee height: | 776 km |
| right ascension of ascending node: | 327.5432° |
| argument of perigee: | 153.8711° |
| revolutions per day: | 14.38442413 |
| mean anomaly at epoch: | 350.3180° |
| orbit number at epoch: | 23585 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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