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 42161U 81053RZ 24227.76066381 .00004393 00000-0 32316-2 0 9991
2 42161 82.9321 243.5163 0056073 159.9100 200.4292 13.94639520 46372
| Epoch (UTC): | 14 August 2024 18:15:21 |
| Eccentricity: | 0.0056073 |
| inclination: | 82.9321° |
| perigee height: | 871 km |
| apogee height: | 953 km |
| right ascension of ascending node: | 243.5163° |
| argument of perigee: | 159.9100° |
| revolutions per day: | 13.94639520 |
| mean anomaly at epoch: | 200.4292° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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