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 39446U 13066AG 22176.39006221 .00001542 00000-0 20413-3 0 9998
2 39446 97.6857 140.1099 0070221 64.0095 296.8328 14.79588017461638
| Epoch (UTC): | 25 June 2022 09:21:41 |
| Eccentricity: | 0.0070221 |
| inclination: | 97.6857° |
| perigee height: | 581 km |
| apogee height: | 680 km |
| right ascension of ascending node: | 140.1099° |
| argument of perigee: | 64.0095° |
| revolutions per day: | 14.79588017 |
| mean anomaly at epoch: | 296.8328° |
| orbit number at epoch: | 46163 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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