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 23028.51197251 .00039865 00000-0 78269-3 0 9994
2 39026 97.2820 23.1604 0026946 70.1959 290.2193 15.46812646563579
| Epoch (UTC): | 28 January 2023 12:17:14 |
| Eccentricity: | 0.0026946 |
| inclination: | 97.2820° |
| perigee height: | 408 km |
| apogee height: | 444 km |
| right ascension of ascending node: | 23.1604° |
| argument of perigee: | 70.1959° |
| revolutions per day: | 15.46812646 |
| mean anomaly at epoch: | 290.2193° |
| orbit number at epoch: | 56357 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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