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 26071.71403103 +.00000000 +00000-0 +10128-4 0 00004
2 16409 82.5412 339.1866 0016155 66.6831 293.6028 13.84923548 05
| Epoch (UTC): | 12 March 2026 17:08:12 |
| Eccentricity: | 0.0016155 |
| inclination: | 82.5412° |
| perigee height: | 935 km |
| apogee height: | 958 km |
| right ascension of ascending node: | 339.1866° |
| argument of perigee: | 66.6831° |
| revolutions per day: | 13.84923548 |
| mean anomaly at epoch: | 293.6028° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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