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 26144.25586242 +.00000000 +00000-0 +00000-0 0 00005
2 40296 63.4432 217.6858 6656956 270.7184 19.5763 2.00590499 03
| Epoch (UTC): | 24 May 2026 06:08:26 |
| Eccentricity: | 0.6656956 |
| inclination: | 63.4432° |
| perigee height: | 2500 km |
| apogee height: | 37859 km |
| right ascension of ascending node: | 217.6858° |
| argument of perigee: | 270.7184° |
| revolutions per day: | 2.00590499 |
| mean anomaly at epoch: | 19.5763° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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