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 23439U 94085A 22175.93555131 -.00000039 00000-0 10000-3 0 9993
2 23439 64.8154 133.5129 0168159 271.2487 86.9179 11.27572660132335
| Epoch (UTC): | 24 June 2022 22:27:11 |
| Eccentricity: | 0.0168159 |
| inclination: | 64.8154° |
| perigee height: | 1881 km |
| apogee height: | 2163 km |
| right ascension of ascending node: | 133.5129° |
| argument of perigee: | 271.2487° |
| revolutions per day: | 11.27572660 |
| mean anomaly at epoch: | 86.9179° |
| orbit number at epoch: | 13233 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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