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 2674U 67011A 23266.79180810 .00008189 00000-0 10992-2 0 9996
2 2674 39.9227 293.7302 0249495 281.2018 76.0813 14.59980701943043
| Epoch (UTC): | 23 September 2023 19:00:12 |
| Eccentricity: | 0.0249495 |
| inclination: | 39.9227° |
| perigee height: | 517 km |
| apogee height: | 869 km |
| right ascension of ascending node: | 293.7302° |
| argument of perigee: | 281.2018° |
| revolutions per day: | 14.59980701 |
| mean anomaly at epoch: | 76.0813° |
| orbit number at epoch: | 94304 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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