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 40042U 26069.59018455 +.00000000 +00000-0 +83865-3 0 00006
2 40042 98.1054 86.7559 0009439 125.5907 234.6212 15.29601396 05
| Epoch (UTC): | 10 March 2026 14:09:51 |
| Eccentricity: | 0.0009439 |
| inclination: | 98.1054° |
| perigee height: | 471 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 86.7559° |
| argument of perigee: | 125.5907° |
| revolutions per day: | 15.29601396 |
| mean anomaly at epoch: | 234.6212° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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