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 22136.88197698 .00003181 00000-0 38387-3 0 9995
2 39444 97.6225 112.2143 0057983 135.3061 225.2848 14.83257034456847
| Epoch (UTC): | 16 May 2022 21:10:02 |
| Eccentricity: | 0.0057983 |
| inclination: | 97.6225° |
| perigee height: | 578 km |
| apogee height: | 659 km |
| right ascension of ascending node: | 112.2143° |
| argument of perigee: | 135.3061° |
| revolutions per day: | 14.83257034 |
| mean anomaly at epoch: | 225.2848° |
| orbit number at epoch: | 45684 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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