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 26069U 00006A 25193.57708927 -.00000132 00000-0 -44439-4 0 9990
2 26069 70.9954 303.4373 0009021 83.8259 276.3891 14.13818733575955
| Epoch (UTC): | 12 July 2025 13:51:00 |
| Eccentricity: | 0.0009021 |
| inclination: | 70.9954° |
| perigee height: | 840 km |
| apogee height: | 853 km |
| right ascension of ascending node: | 303.4373° |
| argument of perigee: | 83.8259° |
| revolutions per day: | 14.13818733 |
| mean anomaly at epoch: | 276.3891° |
| orbit number at epoch: | 57595 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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