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 39026U 12072A 23028.90011737 .00037769 00000-0 74114-3 0 9997
2 39026 97.2819 23.5507 0026886 68.9046 291.5075 15.46841143563632
| Epoch (UTC): | 28 January 2023 21:36:10 |
| Eccentricity: | 0.0026886 |
| inclination: | 97.2819° |
| perigee height: | 407 km |
| apogee height: | 444 km |
| right ascension of ascending node: | 23.5507° |
| argument of perigee: | 68.9046° |
| revolutions per day: | 15.46841143 |
| mean anomaly at epoch: | 291.5075° |
| orbit number at epoch: | 56363 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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