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 16720U 26049.80499936 +.00000000 +00000-0 +55906-4 0 00007
2 16720 82.5563 164.6959 0020747 79.9183 35.7857 14.85648213 01
| Epoch (UTC): | 18 February 2026 19:19:11 |
| Eccentricity: | 0.0020747 |
| inclination: | 82.5563° |
| perigee height: | 597 km |
| apogee height: | 626 km |
| right ascension of ascending node: | 164.6959° |
| argument of perigee: | 79.9183° |
| revolutions per day: | 14.85648213 |
| mean anomaly at epoch: | 35.7857° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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