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 26150.39970830 +.00000000 +00000-0 +14175-3 0 00008
2 40016 97.7559 297.1524 0045933 130.1685 230.3563 14.79515802 07
| Epoch (UTC): | 30 May 2026 09:35:34 |
| Eccentricity: | 0.0045933 |
| inclination: | 97.7559° |
| perigee height: | 599 km |
| apogee height: | 663 km |
| right ascension of ascending node: | 297.1524° |
| argument of perigee: | 130.1685° |
| revolutions per day: | 14.79515802 |
| mean anomaly at epoch: | 230.3563° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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