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 16736U 26022.30560975 +.00000000 +00000-0 +24488-4 0 00003
2 16736 82.5356 46.8194 0011578 275.7916 84.1924 13.84853058 08
| Epoch (UTC): | 22 January 2026 07:20:04 |
| Eccentricity: | 0.0011578 |
| inclination: | 82.5356° |
| perigee height: | 938 km |
| apogee height: | 955 km |
| right ascension of ascending node: | 46.8194° |
| argument of perigee: | 275.7916° |
| revolutions per day: | 13.84853058 |
| mean anomaly at epoch: | 84.1924° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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