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 26040.72549264 +.00000000 +00000-0 +81349-4 0 00009
2 16496 82.5265 286.0587 0076833 6.5988 353.6221 14.86777030 00
| Epoch (UTC): | 09 February 2026 17:24:42 |
| Eccentricity: | 0.0076833 |
| inclination: | 82.5265° |
| perigee height: | 554 km |
| apogee height: | 662 km |
| right ascension of ascending node: | 286.0587° |
| argument of perigee: | 6.5988° |
| revolutions per day: | 14.86777030 |
| mean anomaly at epoch: | 353.6221° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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