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 26106.59690941 +.00000000 +00000-0 +35415-3 0 00002
2 40042 98.0997 127.1245 0007361 19.6989 340.4533 15.31157896 03
| Epoch (UTC): | 16 April 2026 14:19:32 |
| Eccentricity: | 0.0007361 |
| inclination: | 98.0997° |
| perigee height: | 467 km |
| apogee height: | 477 km |
| right ascension of ascending node: | 127.1245° |
| argument of perigee: | 19.6989° |
| revolutions per day: | 15.31157896 |
| mean anomaly at epoch: | 340.4533° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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