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 23036.53219509 .00038634 00000-0 74409-3 0 9991
2 39026 97.2813 31.2254 0025716 44.1037 316.2258 15.47410944564875
| Epoch (UTC): | 05 February 2023 12:46:21 |
| Eccentricity: | 0.0025716 |
| inclination: | 97.2813° |
| perigee height: | 407 km |
| apogee height: | 442 km |
| right ascension of ascending node: | 31.2254° |
| argument of perigee: | 44.1037° |
| revolutions per day: | 15.47410944 |
| mean anomaly at epoch: | 316.2258° |
| orbit number at epoch: | 56487 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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