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 29006U 62047F 24354.54327685 .00001633 00000-0 21703-3 0 9993
2 29006 58.3110 287.9192 0007914 14.3422 345.7844 14.84477829182855
| Epoch (UTC): | 19 December 2024 13:02:19 |
| Eccentricity: | 0.0007914 |
| inclination: | 58.3110° |
| perigee height: | 609 km |
| apogee height: | 621 km |
| right ascension of ascending node: | 287.9192° |
| argument of perigee: | 14.3422° |
| revolutions per day: | 14.84477829 |
| mean anomaly at epoch: | 345.7844° |
| orbit number at epoch: | 18285 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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