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 42957U 17061C 24358.14794760 .00000017 00000-0 -83360-6 0 9997
2 42957 86.3969 251.2436 0001784 77.5275 282.6121 14.34217569377232
| Epoch (UTC): | 23 December 2024 03:33:02 |
| Eccentricity: | 0.0001784 |
| inclination: | 86.3969° |
| perigee height: | 776 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 251.2436° |
| argument of perigee: | 77.5275° |
| revolutions per day: | 14.34217569 |
| mean anomaly at epoch: | 282.6121° |
| orbit number at epoch: | 37723 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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