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 23029.85821085 .00008066 00000-0 88642-3 0 9998
2 39439 97.6650 359.7887 0060409 16.8361 343.4841 14.86549524495658
| Epoch (UTC): | 29 January 2023 20:35:49 |
| Eccentricity: | 0.0060409 |
| inclination: | 97.6650° |
| perigee height: | 566 km |
| apogee height: | 651 km |
| right ascension of ascending node: | 359.7887° |
| argument of perigee: | 16.8361° |
| revolutions per day: | 14.86549524 |
| mean anomaly at epoch: | 343.4841° |
| orbit number at epoch: | 49565 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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