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 26067.16298756 +.00000000 +00000-0 +70959-4 0 00008
2 16720 82.5556 148.4604 0019803 25.8012 349.3049 14.85667270 03
| Epoch (UTC): | 08 March 2026 03:54:42 |
| Eccentricity: | 0.0019803 |
| inclination: | 82.5556° |
| perigee height: | 598 km |
| apogee height: | 625 km |
| right ascension of ascending node: | 148.4604° |
| argument of perigee: | 25.8012° |
| revolutions per day: | 14.85667270 |
| mean anomaly at epoch: | 349.3049° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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