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 16496U 86006B 24281.40680397 .00002927 00000-0 33477-3 0 9997
2 16496 82.5282 27.0629 0017452 254.2562 148.5329 14.85608162 93315
| Epoch (UTC): | 07 October 2024 09:45:47 |
| Eccentricity: | 0.0017452 |
| inclination: | 82.5282° |
| perigee height: | 599 km |
| apogee height: | 624 km |
| right ascension of ascending node: | 27.0629° |
| argument of perigee: | 254.2562° |
| revolutions per day: | 14.85608162 |
| mean anomaly at epoch: | 148.5329° |
| orbit number at epoch: | 9331 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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