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 39439U 13066Z 23081.86510715 .00011584 00000-0 12299-2 0 9995
2 39439 97.6736 50.0304 0057129 200.8571 159.0315 14.87975109504472
| Epoch (UTC): | 22 March 2023 20:45:45 |
| Eccentricity: | 0.0057129 |
| inclination: | 97.6736° |
| perigee height: | 564 km |
| apogee height: | 644 km |
| right ascension of ascending node: | 50.0304° |
| argument of perigee: | 200.8571° |
| revolutions per day: | 14.87975109 |
| mean anomaly at epoch: | 159.0315° |
| orbit number at epoch: | 50447 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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