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 00029U 60002B 24357.69393714 .00001573 00000-0 24747-3 0 9995
2 00029 48.3792 75.7128 0021817 97.4623 262.8770 14.77390066462025
| Epoch (UTC): | 22 December 2024 16:39:16 |
| Eccentricity: | 0.0021817 |
| inclination: | 48.3792° |
| perigee height: | 622 km |
| apogee height: | 653 km |
| right ascension of ascending node: | 75.7128° |
| argument of perigee: | 97.4623° |
| revolutions per day: | 14.77390066 |
| mean anomaly at epoch: | 262.8770° |
| orbit number at epoch: | 46202 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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