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 39430U 13066Q 23029.40528149 .00002841 00000-0 50436-3 0 9990
2 39430 97.7959 288.5820 0148949 52.3485 309.1054 14.60917432489271
| Epoch (UTC): | 29 January 2023 09:43:36 |
| Eccentricity: | 0.0148949 |
| inclination: | 97.7959° |
| perigee height: | 585 km |
| apogee height: | 795 km |
| right ascension of ascending node: | 288.5820° |
| argument of perigee: | 52.3485° |
| revolutions per day: | 14.60917432 |
| mean anomaly at epoch: | 309.1054° |
| orbit number at epoch: | 48927 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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