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 47699U 21015A 24358.19659124 .00000653 00000-0 21731-3 0 9994
2 47699 98.3789 70.8538 0001724 79.2576 280.8807 14.40862336200745
| Epoch (UTC): | 23 December 2024 04:43:05 |
| Eccentricity: | 0.0001724 |
| inclination: | 98.3789° |
| perigee height: | 754 km |
| apogee height: | 757 km |
| right ascension of ascending node: | 70.8538° |
| argument of perigee: | 79.2576° |
| revolutions per day: | 14.40862336 |
| mean anomaly at epoch: | 280.8807° |
| orbit number at epoch: | 20074 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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