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 16909U 26106.05164534 +.00000000 +00000-0 +98670-4 0 00005
2 16909 50.0179 344.3912 0011140 4.1075 142.6410 12.44485698 08
| Epoch (UTC): | 16 April 2026 01:14:22 |
| Eccentricity: | 0.0011140 |
| inclination: | 50.0179° |
| perigee height: | 1479 km |
| apogee height: | 1496 km |
| right ascension of ascending node: | 344.3912° |
| argument of perigee: | 4.1075° |
| revolutions per day: | 12.44485698 |
| mean anomaly at epoch: | 142.6410° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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