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 26106.97590771 +.00000000 +00000-0 +15288-2 0 00004
2 40920 82.4875 117.7848 0010948 119.0421 241.1757 12.42925541 09
| Epoch (UTC): | 16 April 2026 23:25:18 |
| Eccentricity: | 0.0010948 |
| inclination: | 82.4875° |
| perigee height: | 1486 km |
| apogee height: | 1503 km |
| right ascension of ascending node: | 117.7848° |
| argument of perigee: | 119.0421° |
| revolutions per day: | 12.42925541 |
| mean anomaly at epoch: | 241.1757° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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