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 26075.28104134 +.00000000 +00000-0 +68272-3 0 00004
2 40042 98.1041 92.9580 0009601 110.0191 250.2082 15.29865777 03
| Epoch (UTC): | 16 March 2026 06:44:41 |
| Eccentricity: | 0.0009601 |
| inclination: | 98.1041° |
| perigee height: | 470 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 92.9580° |
| argument of perigee: | 110.0191° |
| revolutions per day: | 15.29865777 |
| mean anomaly at epoch: | 250.2082° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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