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 00045U 60007A 22219.10113112 .00000083 00000-0 47992-4 0 9994
2 00045 66.6949 123.4747 0247664 107.9388 254.8880 14.33882247177747
| Epoch (UTC): | 07 August 2022 02:25:37 |
| Eccentricity: | 0.0247664 |
| inclination: | 66.6949° |
| perigee height: | 601 km |
| apogee height: | 956 km |
| right ascension of ascending node: | 123.4747° |
| argument of perigee: | 107.9388° |
| revolutions per day: | 14.33882247 |
| mean anomaly at epoch: | 254.8880° |
| orbit number at epoch: | 17774 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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