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 24258.83072961 .00011103 00000-0 11869-2 0 9992
2 39446 97.7870 206.7615 0056278 285.3259 74.1742 14.87755264582026
| Epoch (UTC): | 14 September 2024 19:56:15 |
| Eccentricity: | 0.0056278 |
| inclination: | 97.7870° |
| perigee height: | 565 km |
| apogee height: | 644 km |
| right ascension of ascending node: | 206.7615° |
| argument of perigee: | 285.3259° |
| revolutions per day: | 14.87755264 |
| mean anomaly at epoch: | 74.1742° |
| orbit number at epoch: | 58202 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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