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 24340.37245834 .00005019 00000-0 69734-3 0 9993
2 39161 97.8082 41.6339 0009470 42.2572 317.9367 14.78267733622367
| Epoch (UTC): | 05 December 2024 08:56:20 |
| Eccentricity: | 0.0009470 |
| inclination: | 97.8082° |
| perigee height: | 628 km |
| apogee height: | 641 km |
| right ascension of ascending node: | 41.6339° |
| argument of perigee: | 42.2572° |
| revolutions per day: | 14.78267733 |
| mean anomaly at epoch: | 317.9367° |
| orbit number at epoch: | 62236 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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