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 38710U 12039D 22322.14595142 .13255880 26334-5 16468-3 0 9999
2 38710 97.4692 57.2581 0008692 273.6939 86.3371 16.49472070581732
| Epoch (UTC): | 18 November 2022 03:30:10 |
| Eccentricity: | 0.0008692 |
| inclination: | 97.4692° |
| perigee height: | 135 km |
| apogee height: | 146 km |
| right ascension of ascending node: | 57.2581° |
| argument of perigee: | 273.6939° |
| revolutions per day: | 16.49472070 |
| mean anomaly at epoch: | 86.3371° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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