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 22175.87130785 .00001978 00000-0 24035-3 0 9998
2 39444 97.6238 149.4390 0056985 10.2942 349.9425 14.83458964462620
| Epoch (UTC): | 24 June 2022 20:54:40 |
| Eccentricity: | 0.0056985 |
| inclination: | 97.6238° |
| perigee height: | 578 km |
| apogee height: | 658 km |
| right ascension of ascending node: | 149.4390° |
| argument of perigee: | 10.2942° |
| revolutions per day: | 14.83458964 |
| mean anomaly at epoch: | 349.9425° |
| orbit number at epoch: | 46262 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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