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 08344U 75094B 25198.66077303 .00000125 00000-0 47644-4 0 9998
2 08344 74.0557 82.5928 0022139 321.5636 38.3941 14.40422801610197
| Epoch (UTC): | 17 July 2025 15:51:30 |
| Eccentricity: | 0.0022139 |
| inclination: | 74.0557° |
| perigee height: | 741 km |
| apogee height: | 773 km |
| right ascension of ascending node: | 82.5928° |
| argument of perigee: | 321.5636° |
| revolutions per day: | 14.40422801 |
| mean anomaly at epoch: | 38.3941° |
| orbit number at epoch: | 61019 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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