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 23339.42923967 .00003646 00000-0 43149-3 0 9997
2 39446 97.7580 289.0059 0064508 137.3263 223.2988 14.83712020539802
| Epoch (UTC): | 05 December 2023 10:18:06 |
| Eccentricity: | 0.0064508 |
| inclination: | 97.7580° |
| perigee height: | 572 km |
| apogee height: | 663 km |
| right ascension of ascending node: | 289.0059° |
| argument of perigee: | 137.3263° |
| revolutions per day: | 14.83712020 |
| mean anomaly at epoch: | 223.2988° |
| orbit number at epoch: | 53980 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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