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 40018U 26156.32954639 +.00000000 +00000-0 +10835-3 0 00007
2 40018 97.9047 289.8190 0064962 237.7720 121.7181 14.74198319 01
| Epoch (UTC): | 05 June 2026 07:54:32 |
| Eccentricity: | 0.0064962 |
| inclination: | 97.9047° |
| perigee height: | 602 km |
| apogee height: | 693 km |
| right ascension of ascending node: | 289.8190° |
| argument of perigee: | 237.7720° |
| revolutions per day: | 14.74198319 |
| mean anomaly at epoch: | 121.7181° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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