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 45598U 98067RL 22058.26358165 .11674468 12483-4 61790-3 0 9999
2 45598 51.6159 103.9349 0001315 314.4869 45.6051 16.42508540104623
| Epoch (UTC): | 27 February 2022 06:19:33 |
| Eccentricity: | 0.0001315 |
| inclination: | 51.6159° |
| perigee height: | 158 km |
| apogee height: | 160 km |
| right ascension of ascending node: | 103.9349° |
| argument of perigee: | 314.4869° |
| revolutions per day: | 16.42508540 |
| mean anomaly at epoch: | 45.6051° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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