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 43617U 18070E 22260.64820158 .15847175 28053-6 19970-3 0 9994
2 43617 92.9902 141.8911 0011446 219.5078 140.5403 16.49147461226007
| Epoch (UTC): | 17 September 2022 15:33:24 |
| Eccentricity: | 0.0011446 |
| inclination: | 92.9902° |
| perigee height: | 134 km |
| apogee height: | 149 km |
| right ascension of ascending node: | 141.8911° |
| argument of perigee: | 219.5078° |
| revolutions per day: | 16.49147461 |
| mean anomaly at epoch: | 140.5403° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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