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 42673U 15069F 24357.92294934 .00002474 00000-0 26754-3 0 9990
2 42673 97.9370 22.2265 0003661 18.7579 341.3772 14.89219373491368
| Epoch (UTC): | 22 December 2024 22:09:02 |
| Eccentricity: | 0.0003661 |
| inclination: | 97.9370° |
| perigee height: | 598 km |
| apogee height: | 603 km |
| right ascension of ascending node: | 22.2265° |
| argument of perigee: | 18.7579° |
| revolutions per day: | 14.89219373 |
| mean anomaly at epoch: | 341.3772° |
| orbit number at epoch: | 49136 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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