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 24255.57783651 .00003113 00000-0 68355-3 0 9992
2 00047 66.6681 334.8433 0230244 251.1632 106.4378 14.43839067357839
| Epoch (UTC): | 11 September 2024 13:52:05 |
| Eccentricity: | 0.0230244 |
| inclination: | 66.6681° |
| perigee height: | 582 km |
| apogee height: | 910 km |
| right ascension of ascending node: | 334.8433° |
| argument of perigee: | 251.1632° |
| revolutions per day: | 14.43839067 |
| mean anomaly at epoch: | 106.4378° |
| orbit number at epoch: | 35783 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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