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 16409U 26069.83561354 +.00000000 +00000-0 +15994-4 0 00003
2 16409 82.5414 340.6819 0016173 71.4547 288.8369 13.84923461 08
| Epoch (UTC): | 10 March 2026 20:03:17 |
| Eccentricity: | 0.0016173 |
| inclination: | 82.5414° |
| perigee height: | 935 km |
| apogee height: | 958 km |
| right ascension of ascending node: | 340.6819° |
| argument of perigee: | 71.4547° |
| revolutions per day: | 13.84923461 |
| mean anomaly at epoch: | 288.8369° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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