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 39161U 13021C 24257.42575688 .00010063 00000-0 14250-2 0 9996
2 39161 97.8208 321.2082 0007655 308.5111 51.5412 14.77226287610153
| Epoch (UTC): | 13 September 2024 10:13:05 |
| Eccentricity: | 0.0007655 |
| inclination: | 97.8208° |
| perigee height: | 633 km |
| apogee height: | 643 km |
| right ascension of ascending node: | 321.2082° |
| argument of perigee: | 308.5111° |
| revolutions per day: | 14.77226287 |
| mean anomaly at epoch: | 51.5412° |
| orbit number at epoch: | 61015 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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