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 39421U 13066F 23081.53741289 .00004630 00000-0 47760-3 0 9998
2 39421 97.5308 66.5382 0031405 98.6263 261.8516 14.90292208506580
| Epoch (UTC): | 22 March 2023 12:53:52 |
| Eccentricity: | 0.0031405 |
| inclination: | 97.5308° |
| perigee height: | 575 km |
| apogee height: | 619 km |
| right ascension of ascending node: | 66.5382° |
| argument of perigee: | 98.6263° |
| revolutions per day: | 14.90292208 |
| mean anomaly at epoch: | 261.8516° |
| orbit number at epoch: | 50658 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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