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 40296U 26109.85725125 +.00000000 +00000-0 +00000-0 0 00007
2 40296 63.4485 221.0984 6669524 270.9422 19.3446 2.00584616 02
| Epoch (UTC): | 19 April 2026 20:34:26 |
| Eccentricity: | 0.6669524 |
| inclination: | 63.4485° |
| perigee height: | 2467 km |
| apogee height: | 37894 km |
| right ascension of ascending node: | 221.0984° |
| argument of perigee: | 270.9422° |
| revolutions per day: | 2.00584616 |
| mean anomaly at epoch: | 19.3446° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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