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 40147U 26145.45933352 +.00000000 +00000-0 +00000-0 0 00001
2 40147 0.0555 53.5178 0003286 358.4789 87.9334 1.00272005 06
| Epoch (UTC): | 25 May 2026 11:01:26 |
| Eccentricity: | 0.0003286 |
| inclination: | 0.0555° |
| perigee height: | 35773 km |
| apogee height: | 35800 km |
| right ascension of ascending node: | 53.5178° |
| argument of perigee: | 358.4789° |
| revolutions per day: | 1.00272005 |
| mean anomaly at epoch: | 87.9334° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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