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 23265.83202237 .00006653 00000-0 79863-3 0 9993
2 39446 97.7437 217.5801 0065380 21.2370 339.1535 14.82791905528893
| Epoch (UTC): | 22 September 2023 19:58:06 |
| Eccentricity: | 0.0065380 |
| inclination: | 97.7437° |
| perigee height: | 575 km |
| apogee height: | 666 km |
| right ascension of ascending node: | 217.5801° |
| argument of perigee: | 21.2370° |
| revolutions per day: | 14.82791905 |
| mean anomaly at epoch: | 339.1535° |
| orbit number at epoch: | 52889 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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