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 16494U 26136.82719446 +.00000000 +00000-0 +13181-3 0 00003
2 16494 82.9317 169.9280 0020708 130.5306 42.8008 13.76785391 08
| Epoch (UTC): | 16 May 2026 19:51:09 |
| Eccentricity: | 0.0020708 |
| inclination: | 82.9317° |
| perigee height: | 960 km |
| apogee height: | 991 km |
| right ascension of ascending node: | 169.9280° |
| argument of perigee: | 130.5306° |
| revolutions per day: | 13.76785391 |
| mean anomaly at epoch: | 42.8008° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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