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 26145.66550185 +.00000000 +00000-0 +95740-4 0 00007
2 40016 97.7555 292.5836 0045690 145.2160 215.2053 14.79505352 08
| Epoch (UTC): | 25 May 2026 15:58:19 |
| Eccentricity: | 0.0045690 |
| inclination: | 97.7555° |
| perigee height: | 599 km |
| apogee height: | 663 km |
| right ascension of ascending node: | 292.5836° |
| argument of perigee: | 145.2160° |
| revolutions per day: | 14.79505352 |
| mean anomaly at epoch: | 215.2053° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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