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 16882U 86055B 25198.51533505 .00000372 00000-0 40333-4 0 9990
2 16882 82.5217 347.6464 0019868 33.9584 33.0547 14.85324012105626
| Epoch (UTC): | 17 July 2025 12:22:04 |
| Eccentricity: | 0.0019868 |
| inclination: | 82.5217° |
| perigee height: | 598 km |
| apogee height: | 626 km |
| right ascension of ascending node: | 347.6464° |
| argument of perigee: | 33.9584° |
| revolutions per day: | 14.85324012 |
| mean anomaly at epoch: | 33.0547° |
| orbit number at epoch: | 10562 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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