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 26066.15102431 +.00000000 +00000-0 +38701-4 0 00003
2 16409 82.5416 343.6146 0016237 81.0125 279.2872 13.84923302 03
| Epoch (UTC): | 07 March 2026 03:37:28 |
| Eccentricity: | 0.0016237 |
| inclination: | 82.5416° |
| perigee height: | 935 km |
| apogee height: | 958 km |
| right ascension of ascending node: | 343.6146° |
| argument of perigee: | 81.0125° |
| revolutions per day: | 13.84923302 |
| mean anomaly at epoch: | 279.2872° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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