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 16791U 86046A 24257.17241043 .00017722 00000-0 93473-3 0 9998
2 16791 82.4663 326.4014 0018956 68.6329 291.6923 15.15291367 83898
| Epoch (UTC): | 13 September 2024 04:08:16 |
| Eccentricity: | 0.0018956 |
| inclination: | 82.4663° |
| perigee height: | 507 km |
| apogee height: | 533 km |
| right ascension of ascending node: | 326.4014° |
| argument of perigee: | 68.6329° |
| revolutions per day: | 15.15291367 |
| mean anomaly at epoch: | 291.6923° |
| orbit number at epoch: | 8389 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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