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 25191.59941314 .00001675 00000-0 11681-3 0 9997
2 26474 67.9893 0.0090 0046947 308.6628 51.0323 15.07322828356409
| Epoch (UTC): | 10 July 2025 14:23:09 |
| Eccentricity: | 0.0046947 |
| inclination: | 67.9893° |
| perigee height: | 512 km |
| apogee height: | 577 km |
| right ascension of ascending node: | 0.0090° |
| argument of perigee: | 308.6628° |
| revolutions per day: | 15.07322828 |
| mean anomaly at epoch: | 51.0323° |
| orbit number at epoch: | 35640 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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