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 23079.45908689 .00005984 00000-0 67911-3 0 9993
2 39444 97.6621 46.8168 0053121 203.4326 156.4469 14.85655495502466
| Epoch (UTC): | 20 March 2023 11:01:05 |
| Eccentricity: | 0.0053121 |
| inclination: | 97.6621° |
| perigee height: | 574 km |
| apogee height: | 648 km |
| right ascension of ascending node: | 46.8168° |
| argument of perigee: | 203.4326° |
| revolutions per day: | 14.85655495 |
| mean anomaly at epoch: | 156.4469° |
| orbit number at epoch: | 50246 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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