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 23335.85486806 .00006234 00000-0 73381-3 0 9993
2 39446 97.7585 285.5328 0064141 148.8697 211.6343 14.83676212539277
| Epoch (UTC): | 01 December 2023 20:31:00 |
| Eccentricity: | 0.0064141 |
| inclination: | 97.7585° |
| perigee height: | 573 km |
| apogee height: | 662 km |
| right ascension of ascending node: | 285.5328° |
| argument of perigee: | 148.8697° |
| revolutions per day: | 14.83676212 |
| mean anomaly at epoch: | 211.6343° |
| orbit number at epoch: | 53927 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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