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 40016U 26075.19118578 +.00000000 +00000-0 +10873-3 0 00006
2 40016 97.7425 224.6220 0045246 17.8424 342.4365 14.79402653 00
| Epoch (UTC): | 16 March 2026 04:35:18 |
| Eccentricity: | 0.0045246 |
| inclination: | 97.7425° |
| perigee height: | 599 km |
| apogee height: | 663 km |
| right ascension of ascending node: | 224.6220° |
| argument of perigee: | 17.8424° |
| revolutions per day: | 14.79402653 |
| mean anomaly at epoch: | 342.4365° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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