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 23031.48757416 .00035956 00000-0 70164-3 0 9992
2 39026 97.2816 26.1520 0026564 60.5166 299.8728 15.47022272564033
| Epoch (UTC): | 31 January 2023 11:42:06 |
| Eccentricity: | 0.0026564 |
| inclination: | 97.2816° |
| perigee height: | 407 km |
| apogee height: | 443 km |
| right ascension of ascending node: | 26.1520° |
| argument of perigee: | 60.5166° |
| revolutions per day: | 15.47022272 |
| mean anomaly at epoch: | 299.8728° |
| orbit number at epoch: | 56403 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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