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 26020.17392645 +.00000000 +00000-0 +14875-3 0 00002
2 16494 82.9298 256.7224 0020711 98.7344 19.9283 13.76777145 08
| Epoch (UTC): | 20 January 2026 04:10:27 |
| Eccentricity: | 0.0020711 |
| inclination: | 82.9298° |
| perigee height: | 960 km |
| apogee height: | 991 km |
| right ascension of ascending node: | 256.7224° |
| argument of perigee: | 98.7344° |
| revolutions per day: | 13.76777145 |
| mean anomaly at epoch: | 19.9283° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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