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 26931U 01043C 25200.81287570 .00000092 00000-0 65439-4 0 9998
2 26931 67.0511 23.8147 0006317 276.8600 83.1783 14.31750017242865
| Epoch (UTC): | 19 July 2025 19:30:32 |
| Eccentricity: | 0.0006317 |
| inclination: | 67.0511° |
| perigee height: | 781 km |
| apogee height: | 790 km |
| right ascension of ascending node: | 23.8147° |
| argument of perigee: | 276.8600° |
| revolutions per day: | 14.31750017 |
| mean anomaly at epoch: | 83.1783° |
| orbit number at epoch: | 24286 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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