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 is defined by the following mean orbital elements,
1 47964U 21022AJ 24210.04111032 .13699809 26224-5 63394-3 0 9992
2 47964 97.4268 125.0774 0011420 232.5879 127.4383 16.42108858184709
| Epoch (UTC): | 28 July 2024 00:59:11 |
| Eccentricity: | 0.0011420 |
| inclination: | 97.4268° |
| perigee height: | 153 km |
| apogee height: | 167 km |
| right ascension of ascending node: | 125.0774° |
| argument of perigee: | 232.5879° |
| revolutions per day: | 16.42108858 |
| mean anomaly at epoch: | 127.4383° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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