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 23153.47410965 -.00000089 00000-0 -20519-4 0 9992
2 22220 70.9985 157.9703 0013706 205.9429 264.1820 14.16565331578613
| Epoch (UTC): | 02 June 2023 11:22:43 |
| Eccentricity: | 0.0013706 |
| inclination: | 70.9985° |
| perigee height: | 827 km |
| apogee height: | 847 km |
| right ascension of ascending node: | 157.9703° |
| argument of perigee: | 205.9429° |
| revolutions per day: | 14.16565331 |
| mean anomaly at epoch: | 264.1820° |
| orbit number at epoch: | 57861 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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