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 data is extracted from the following two-line orbital elements,
1 22220U 92076B 23152.48588959 -.00000032 00000-0 81319-5 0 9994
2 22220 70.9985 160.0509 0013759 207.3079 264.7588 14.16565366578476
| Epoch (UTC): | 01 June 2023 11:39:40 |
| Eccentricity: | 0.0013759 |
| inclination: | 70.9985° |
| perigee height: | 827 km |
| apogee height: | 847 km |
| right ascension of ascending node: | 160.0509° |
| argument of perigee: | 207.3079° |
| revolutions per day: | 14.16565366 |
| mean anomaly at epoch: | 264.7588° |
| orbit number at epoch: | 57847 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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