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 39061U 13002A 23249.98287803 0.00000000 00000-0 00000-0 0 03
2 39061 97.4393 10.5018 0003883 55.7955 304.1329 15.17657496 02
| Epoch (UTC): | 06 September 2023 23:35:20 |
| Eccentricity: | 0.0003883 |
| inclination: | 97.4393° |
| perigee height: | 510 km |
| apogee height: | 515 km |
| right ascension of ascending node: | 10.5018° |
| argument of perigee: | 55.7955° |
| revolutions per day: | 15.17657496 |
| mean anomaly at epoch: | 304.1329° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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