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 23090.84092588 .00006101 00000-0 75779-3 0 9996
2 39446 97.7259 48.4044 0064671 230.9476 128.5971 14.81457305503566
| Epoch (UTC): | 31 March 2023 20:10:55 |
| Eccentricity: | 0.0064671 |
| inclination: | 97.7259° |
| perigee height: | 579 km |
| apogee height: | 670 km |
| right ascension of ascending node: | 48.4044° |
| argument of perigee: | 230.9476° |
| revolutions per day: | 14.81457305 |
| mean anomaly at epoch: | 128.5971° |
| orbit number at epoch: | 50356 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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