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 26044.59072257 +.00000000 +00000-0 +64354-3 0 00001
2 40042 98.1062 59.5376 0006730 205.6403 154.4502 15.28489046 07
| Epoch (UTC): | 13 February 2026 14:10:38 |
| Eccentricity: | 0.0006730 |
| inclination: | 98.1062° |
| perigee height: | 476 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 59.5376° |
| argument of perigee: | 205.6403° |
| revolutions per day: | 15.28489046 |
| mean anomaly at epoch: | 154.4502° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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