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 is defined by the following mean orbital elements,
1 16682U 26160.21090352 +.00000000 +00000-0 +88494-4 0 00000
2 16682 74.0255 320.5418 0014898 226.5374 311.1716 14.37348006 06
| Epoch (UTC): | 09 June 2026 05:03:42 |
| Eccentricity: | 0.0014898 |
| inclination: | 74.0255° |
| perigee height: | 757 km |
| apogee height: | 778 km |
| right ascension of ascending node: | 320.5418° |
| argument of perigee: | 226.5374° |
| revolutions per day: | 14.37348006 |
| mean anomaly at epoch: | 311.1716° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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