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 23080.30382927 .00005298 00000-0 66125-3 0 9996
2 39446 97.7248 38.2423 0064491 266.3199 93.0637 14.81329808502006
| Epoch (UTC): | 21 March 2023 07:17:30 |
| Eccentricity: | 0.0064491 |
| inclination: | 97.7248° |
| perigee height: | 580 km |
| apogee height: | 670 km |
| right ascension of ascending node: | 38.2423° |
| argument of perigee: | 266.3199° |
| revolutions per day: | 14.81329808 |
| mean anomaly at epoch: | 93.0637° |
| orbit number at epoch: | 50200 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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