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 26145.33377784 +.00000000 +00000-0 +75924-4 0 00007
2 40018 97.9029 279.0950 0064742 273.8440 85.5368 14.74181400 09
| Epoch (UTC): | 25 May 2026 08:00:38 |
| Eccentricity: | 0.0064742 |
| inclination: | 97.9029° |
| perigee height: | 602 km |
| apogee height: | 693 km |
| right ascension of ascending node: | 279.0950° |
| argument of perigee: | 273.8440° |
| revolutions per day: | 14.74181400 |
| mean anomaly at epoch: | 85.5368° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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