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 26474U 00047B 25189.54236101 .00001817 00000-0 12604-3 0 9994
2 26474 67.9904 5.7734 0046828 310.8437 48.8655 15.07315832356094
| Epoch (UTC): | 08 July 2025 13:00:59 |
| Eccentricity: | 0.0046828 |
| inclination: | 67.9904° |
| perigee height: | 512 km |
| apogee height: | 577 km |
| right ascension of ascending node: | 5.7734° |
| argument of perigee: | 310.8437° |
| revolutions per day: | 15.07315832 |
| mean anomaly at epoch: | 48.8655° |
| orbit number at epoch: | 35609 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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