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 23037.50216405 .00047303 00000-0 90712-3 0 9999
2 39026 97.2817 32.2015 0025510 40.9910 319.3251 15.47498639564965
| Epoch (UTC): | 06 February 2023 12:03:06 |
| Eccentricity: | 0.0025510 |
| inclination: | 97.2817° |
| perigee height: | 407 km |
| apogee height: | 441 km |
| right ascension of ascending node: | 32.2015° |
| argument of perigee: | 40.9910° |
| revolutions per day: | 15.47498639 |
| mean anomaly at epoch: | 319.3251° |
| orbit number at epoch: | 56496 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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