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 25194.50541050 .00000573 00000-0 58786-4 0 9990
2 16496 82.5282 124.7427 0076800 346.6830 13.2356 14.86395694134758
| Epoch (UTC): | 13 July 2025 12:07:47 |
| Eccentricity: | 0.0076800 |
| inclination: | 82.5282° |
| perigee height: | 555 km |
| apogee height: | 663 km |
| right ascension of ascending node: | 124.7427° |
| argument of perigee: | 346.6830° |
| revolutions per day: | 14.86395694 |
| mean anomaly at epoch: | 13.2356° |
| orbit number at epoch: | 13475 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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