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 26076.19333253 +.00000000 +00000-0 +28921-4 0 00009
2 16409 82.5407 335.6210 0016017 54.9501 305.3160 13.84923870 00
| Epoch (UTC): | 17 March 2026 04:38:23 |
| Eccentricity: | 0.0016017 |
| inclination: | 82.5407° |
| perigee height: | 935 km |
| apogee height: | 958 km |
| right ascension of ascending node: | 335.6210° |
| argument of perigee: | 54.9501° |
| revolutions per day: | 13.84923870 |
| mean anomaly at epoch: | 305.3160° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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