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 57929C 23147S 24358.15118056 .00026524 00000+0 85006-3 0 3587
2 57929 42.9982 150.9348 0006275 315.9003 186.2028 15.31494410 19
| Epoch (UTC): | 23 December 2024 03:37:42 |
| Eccentricity: | 0.0006275 |
| inclination: | 42.9982° |
| perigee height: | 467 km |
| apogee height: | 475 km |
| right ascension of ascending node: | 150.9348° |
| argument of perigee: | 315.9003° |
| revolutions per day: | 15.31494410 |
| mean anomaly at epoch: | 186.2028° |
| orbit number at epoch: | 1 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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