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 25341.30693090 .00006083 00000-0 38804-3 0 9992
2 26474 67.9905 300.1119 0039387 151.2344 209.0989 15.08720353378971
| Epoch (UTC): | 07 December 2025 07:21:58 |
| Eccentricity: | 0.0039387 |
| inclination: | 67.9905° |
| perigee height: | 513 km |
| apogee height: | 567 km |
| right ascension of ascending node: | 300.1119° |
| argument of perigee: | 151.2344° |
| revolutions per day: | 15.08720353 |
| mean anomaly at epoch: | 209.0989° |
| orbit number at epoch: | 37897 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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