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 40057U 26118.55028263 +.00000000 +00000-0 +59704-3 0 00006
2 40057 98.2594 20.7470 0009585 78.0479 282.1816 14.97421323 01
| Epoch (UTC): | 28 April 2026 13:12:24 |
| Eccentricity: | 0.0009585 |
| inclination: | 98.2594° |
| perigee height: | 568 km |
| apogee height: | 582 km |
| right ascension of ascending node: | 20.7470° |
| argument of perigee: | 78.0479° |
| revolutions per day: | 14.97421323 |
| mean anomaly at epoch: | 282.1816° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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