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 22141.87402653 .00004645 00000-0 55681-3 0 9992
2 39444 97.6224 116.9796 0058352 119.3223 241.3839 14.83296659457581
| Epoch (UTC): | 21 May 2022 20:58:35 |
| Eccentricity: | 0.0058352 |
| inclination: | 97.6224° |
| perigee height: | 578 km |
| apogee height: | 660 km |
| right ascension of ascending node: | 116.9796° |
| argument of perigee: | 119.3223° |
| revolutions per day: | 14.83296659 |
| mean anomaly at epoch: | 241.3839° |
| orbit number at epoch: | 45758 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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