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 23086.85583728 .00004601 00000-0 57395-3 0 9990
2 39446 97.7264 44.5614 0064506 244.3084 115.1459 14.81411438502382
| Epoch (UTC): | 27 March 2023 20:32:24 |
| Eccentricity: | 0.0064506 |
| inclination: | 97.7264° |
| perigee height: | 580 km |
| apogee height: | 670 km |
| right ascension of ascending node: | 44.5614° |
| argument of perigee: | 244.3084° |
| revolutions per day: | 14.81411438 |
| mean anomaly at epoch: | 115.1459° |
| orbit number at epoch: | 50238 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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