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 23150.13971815 .00000097 00000-0 72520-4 0 9994
2 22220 70.9984 164.9906 0013874 210.4192 180.6001 14.16565012578472
| Epoch (UTC): | 30 May 2023 03:21:11 |
| Eccentricity: | 0.0013874 |
| inclination: | 70.9984° |
| perigee height: | 827 km |
| apogee height: | 847 km |
| right ascension of ascending node: | 164.9906° |
| argument of perigee: | 210.4192° |
| revolutions per day: | 14.16565012 |
| mean anomaly at epoch: | 180.6001° |
| 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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