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 39444U 13066AE 23150.42539612 .00003997 00000-0 44628-3 0 9998
2 39444 97.6700 115.2472 0052322 333.3456 26.5072 14.86548204513001
| Epoch (UTC): | 30 May 2023 10:12:34 |
| Eccentricity: | 0.0052322 |
| inclination: | 97.6700° |
| perigee height: | 572 km |
| apogee height: | 645 km |
| right ascension of ascending node: | 115.2472° |
| argument of perigee: | 333.3456° |
| revolutions per day: | 14.86548204 |
| mean anomaly at epoch: | 26.5072° |
| orbit number at epoch: | 51300 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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