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 39360U 13058A 22222.15628896 -.00000028 00000-0 00000+0 0 9993
2 39360 0.0537 268.6880 0000553 106.8220 243.1915 1.00269409 32234
| Epoch (UTC): | 10 August 2022 03:45:03 |
| Eccentricity: | 0.0000553 |
| inclination: | 0.0537° |
| perigee height: | 35784 km |
| apogee height: | 35789 km |
| right ascension of ascending node: | 268.6880° |
| argument of perigee: | 106.8220° |
| revolutions per day: | 1.00269409 |
| mean anomaly at epoch: | 243.1915° |
| orbit number at epoch: | 3223 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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