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 26071.68757025 +.00000000 +00000-0 +23915-3 0 00006
2 16791 82.4608 140.5439 0012895 327.3948 32.6492 15.25743066 06
| Epoch (UTC): | 12 March 2026 16:30:06 |
| Eccentricity: | 0.0012895 |
| inclination: | 82.4608° |
| perigee height: | 480 km |
| apogee height: | 497 km |
| right ascension of ascending node: | 140.5439° |
| argument of perigee: | 327.3948° |
| revolutions per day: | 15.25743066 |
| mean anomaly at epoch: | 32.6492° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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