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 39446U 13066AG 24252.84453837 .00014681 00000-0 15728-2 0 9994
2 39446 97.7863 200.8845 0056818 305.6220 53.9711 14.87574885581132
| Epoch (UTC): | 08 September 2024 20:16:08 |
| Eccentricity: | 0.0056818 |
| inclination: | 97.7863° |
| perigee height: | 566 km |
| apogee height: | 645 km |
| right ascension of ascending node: | 200.8845° |
| argument of perigee: | 305.6220° |
| revolutions per day: | 14.87574885 |
| mean anomaly at epoch: | 53.9711° |
| orbit number at epoch: | 58113 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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