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 24251.83555939 .00015646 00000-0 16766-2 0 9993
2 39446 97.7865 199.8943 0056892 309.0915 50.5248 14.87546562580982
| Epoch (UTC): | 07 September 2024 20:03:12 |
| Eccentricity: | 0.0056892 |
| inclination: | 97.7865° |
| perigee height: | 566 km |
| apogee height: | 645 km |
| right ascension of ascending node: | 199.8943° |
| argument of perigee: | 309.0915° |
| revolutions per day: | 14.87546562 |
| mean anomaly at epoch: | 50.5248° |
| orbit number at epoch: | 58098 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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