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 26161.52581147 +.00000000 +00000-0 +15007-3 0 00002
2 16494 82.9306 151.5510 0020918 65.9236 55.5522 13.76792940 05
| Epoch (UTC): | 10 June 2026 12:37:10 |
| Eccentricity: | 0.0020918 |
| inclination: | 82.9306° |
| perigee height: | 960 km |
| apogee height: | 991 km |
| right ascension of ascending node: | 151.5510° |
| argument of perigee: | 65.9236° |
| revolutions per day: | 13.76792940 |
| mean anomaly at epoch: | 55.5522° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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