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 40086U 26145.49720373 +.00000000 +00000-0 +81619-4 0 00003
2 40086 47.0018 198.7618 0000938 164.5350 195.5564 14.58815802 01
| Epoch (UTC): | 25 May 2026 11:55:58 |
| Eccentricity: | 0.0000938 |
| inclination: | 47.0018° |
| perigee height: | 696 km |
| apogee height: | 698 km |
| right ascension of ascending node: | 198.7618° |
| argument of perigee: | 164.5350° |
| revolutions per day: | 14.58815802 |
| mean anomaly at epoch: | 195.5564° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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