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 26041.94829083 +.00000000 +00000-0 +25294-4 0 00005
2 16409 82.5395 2.8810 0015650 143.9683 216.2536 13.84922126 07
| Epoch (UTC): | 10 February 2026 22:45:32 |
| Eccentricity: | 0.0015650 |
| inclination: | 82.5395° |
| perigee height: | 935 km |
| apogee height: | 958 km |
| right ascension of ascending node: | 2.8810° |
| argument of perigee: | 143.9683° |
| revolutions per day: | 13.84922126 |
| mean anomaly at epoch: | 216.2536° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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