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 40920U 26156.80202035 +.00000000 +00000-0 +58931-3 0 00007
2 40920 82.4924 86.7584 0010664 20.4475 339.7029 12.42926633 04
| Epoch (UTC): | 05 June 2026 19:14:54 |
| Eccentricity: | 0.0010664 |
| inclination: | 82.4924° |
| perigee height: | 1486 km |
| apogee height: | 1503 km |
| right ascension of ascending node: | 86.7584° |
| argument of perigee: | 20.4475° |
| revolutions per day: | 12.42926633 |
| mean anomaly at epoch: | 339.7029° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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