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 26158.94660661 +.00000000 +00000-0 +10739-3 0 00009
2 16682 74.0254 322.8696 0014941 229.0657 249.2316 14.37347580 02
| Epoch (UTC): | 07 June 2026 22:43:06 |
| Eccentricity: | 0.0014941 |
| inclination: | 74.0254° |
| perigee height: | 757 km |
| apogee height: | 778 km |
| right ascension of ascending node: | 322.8696° |
| argument of perigee: | 229.0657° |
| revolutions per day: | 14.37347580 |
| mean anomaly at epoch: | 249.2316° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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