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 43616U 18070D 22273.19173268 .15406410 25966-6 24527-3 0 9997
2 43616 92.9806 145.7922 0009909 241.3990 118.6326 16.47871482227917
| Epoch (UTC): | 30 September 2022 04:36:05 |
| Eccentricity: | 0.0009909 |
| inclination: | 92.9806° |
| perigee height: | 138 km |
| apogee height: | 151 km |
| right ascension of ascending node: | 145.7922° |
| argument of perigee: | 241.3990° |
| revolutions per day: | 16.47871482 |
| mean anomaly at epoch: | 118.6326° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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