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 16728U 26088.21942097 +.00000000 +00000-0 +11351-3 0 00009
2 16728 82.9516 118.8086 0029635 226.5104 203.6729 13.77074268 08
| Epoch (UTC): | 29 March 2026 05:15:57 |
| Eccentricity: | 0.0029635 |
| inclination: | 82.9516° |
| perigee height: | 952 km |
| apogee height: | 996 km |
| right ascension of ascending node: | 118.8086° |
| argument of perigee: | 226.5104° |
| revolutions per day: | 13.77074268 |
| mean anomaly at epoch: | 203.6729° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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