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 40061U 26103.97624522 +.00000000 +00000-0 -40137-3 0 00002
2 40061 82.5154 347.4768 0029185 290.6625 69.1326 12.42982967 09
| Epoch (UTC): | 13 April 2026 23:25:47 |
| Eccentricity: | 0.0029185 |
| inclination: | 82.5154° |
| perigee height: | 1471 km |
| apogee height: | 1517 km |
| right ascension of ascending node: | 347.4768° |
| argument of perigee: | 290.6625° |
| revolutions per day: | 12.42982967 |
| mean anomaly at epoch: | 69.1326° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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