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 00047U 60007C 24256.61687819 .00004633 00000-0 10051-2 0 9994
2 00047 66.6680 332.0569 0230169 250.4250 107.1875 14.43851320357984
| Epoch (UTC): | 12 September 2024 14:48:18 |
| Eccentricity: | 0.0230169 |
| inclination: | 66.6680° |
| perigee height: | 582 km |
| apogee height: | 910 km |
| right ascension of ascending node: | 332.0569° |
| argument of perigee: | 250.4250° |
| revolutions per day: | 14.43851320 |
| mean anomaly at epoch: | 107.1875° |
| orbit number at epoch: | 35798 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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