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 26074.93788433 +.00000000 +00000-0 +40580-4 0 00004
2 16720 82.5542 141.1864 0019117 0.4619 172.2809 14.85674165 04
| Epoch (UTC): | 15 March 2026 22:30:33 |
| Eccentricity: | 0.0019117 |
| inclination: | 82.5542° |
| perigee height: | 598 km |
| apogee height: | 625 km |
| right ascension of ascending node: | 141.1864° |
| argument of perigee: | 0.4619° |
| revolutions per day: | 14.85674165 |
| mean anomaly at epoch: | 172.2809° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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