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 39444U 13066AE 22180.86265259 .00001283 00000-0 15818-3 0 9996
2 39444 97.6247 154.2061 0056488 353.9179 6.1343 14.83475147463361
| Epoch (UTC): | 29 June 2022 20:42:13 |
| Eccentricity: | 0.0056488 |
| inclination: | 97.6247° |
| perigee height: | 579 km |
| apogee height: | 658 km |
| right ascension of ascending node: | 154.2061° |
| argument of perigee: | 353.9179° |
| revolutions per day: | 14.83475147 |
| mean anomaly at epoch: | 6.1343° |
| orbit number at epoch: | 46336 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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