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 31601U 07025A 21276.14299526 0.00004800 00000-0 16540-3 0 05
2 31601 141.7093 180.6944 0005498 249.2591 110.7401 15.29099636 02
| Epoch (UTC): | 03 October 2021 03:25:54 |
| Eccentricity: | 0.0005498 |
| inclination: | 141.7093° |
| perigee height: | 475 km |
| apogee height: | 482 km |
| right ascension of ascending node: | 180.6944° |
| argument of perigee: | 249.2591° |
| revolutions per day: | 15.29099636 |
| mean anomaly at epoch: | 110.7401° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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