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 26040.18708731 +.00000000 +00000-0 +87664-4 0 00001
2 16496 82.5265 286.5653 0076879 8.3686 351.8791 14.86776467 09
| Epoch (UTC): | 09 February 2026 04:29:24 |
| Eccentricity: | 0.0076879 |
| inclination: | 82.5265° |
| perigee height: | 554 km |
| apogee height: | 662 km |
| right ascension of ascending node: | 286.5653° |
| argument of perigee: | 8.3686° |
| revolutions per day: | 14.86776467 |
| mean anomaly at epoch: | 351.8791° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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