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 26134.78391832 +.00000000 +00000-0 +00000-0 0 00001
2 40296 63.4426 218.6194 6660363 270.7867 19.5320 2.00588881 06
| Epoch (UTC): | 14 May 2026 18:48:50 |
| Eccentricity: | 0.6660363 |
| inclination: | 63.4426° |
| perigee height: | 2491 km |
| apogee height: | 37869 km |
| right ascension of ascending node: | 218.6194° |
| argument of perigee: | 270.7867° |
| revolutions per day: | 2.00588881 |
| mean anomaly at epoch: | 19.5320° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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