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 16496U 26039.17757699 +.00000000 +00000-0 +89866-4 0 00001
2 16496 82.5268 287.5152 0076973 11.6997 348.5985 14.86774656 00
| Epoch (UTC): | 08 February 2026 04:15:42 |
| Eccentricity: | 0.0076973 |
| inclination: | 82.5268° |
| perigee height: | 554 km |
| apogee height: | 662 km |
| right ascension of ascending node: | 287.5152° |
| argument of perigee: | 11.6997° |
| revolutions per day: | 14.86774656 |
| mean anomaly at epoch: | 348.5985° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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