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 39492U 13078C 24337.47415681 .00005454 00000-0 51911-3 0 9999
2 39492 82.4170 93.9427 0017770 1.2592 358.8670 14.93141302593660
| Epoch (UTC): | 02 December 2024 11:22:47 |
| Eccentricity: | 0.0017770 |
| inclination: | 82.4170° |
| perigee height: | 576 km |
| apogee height: | 600 km |
| right ascension of ascending node: | 93.9427° |
| argument of perigee: | 1.2592° |
| revolutions per day: | 14.93141302 |
| mean anomaly at epoch: | 358.8670° |
| orbit number at epoch: | 59366 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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