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 26072.29129481 +.00000000 +00000-0 +51424-4 0 00002
2 16720 82.5548 143.6627 0019360 9.1772 57.2444 14.85672157 06
| Epoch (UTC): | 13 March 2026 06:59:27 |
| Eccentricity: | 0.0019360 |
| inclination: | 82.5548° |
| perigee height: | 598 km |
| apogee height: | 625 km |
| right ascension of ascending node: | 143.6627° |
| argument of perigee: | 9.1772° |
| revolutions per day: | 14.85672157 |
| mean anomaly at epoch: | 57.2444° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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