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 24280.92959325 .00002780 00000-0 61379-3 0 9990
2 00047 66.6647 266.8496 0228808 233.1036 124.8909 14.43952918361497
| Epoch (UTC): | 06 October 2024 22:18:36 |
| Eccentricity: | 0.0228808 |
| inclination: | 66.6647° |
| perigee height: | 582 km |
| apogee height: | 908 km |
| right ascension of ascending node: | 266.8496° |
| argument of perigee: | 233.1036° |
| revolutions per day: | 14.43952918 |
| mean anomaly at epoch: | 124.8909° |
| orbit number at epoch: | 36149 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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