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 16791U 26073.58948372 +.00000000 +00000-0 +30699-3 0 00001
2 16791 82.4608 138.6271 0012684 320.1090 39.9214 15.25769781 07
| Epoch (UTC): | 14 March 2026 14:08:51 |
| Eccentricity: | 0.0012684 |
| inclination: | 82.4608° |
| perigee height: | 480 km |
| apogee height: | 497 km |
| right ascension of ascending node: | 138.6271° |
| argument of perigee: | 320.1090° |
| revolutions per day: | 15.25769781 |
| mean anomaly at epoch: | 39.9214° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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