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 24263.45409371 .00004332 00000-0 61702-3 0 9998
2 39161 97.8197 327.0538 0007480 285.7213 74.3172 14.77289544611045
| Epoch (UTC): | 19 September 2024 10:53:53 |
| Eccentricity: | 0.0007480 |
| inclination: | 97.8197° |
| perigee height: | 632 km |
| apogee height: | 643 km |
| right ascension of ascending node: | 327.0538° |
| argument of perigee: | 285.7213° |
| revolutions per day: | 14.77289544 |
| mean anomaly at epoch: | 74.3172° |
| orbit number at epoch: | 61104 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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