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 40136U 26145.60143037 +.00000000 +00000-0 +70619-4 0 00006
2 40136 98.7061 147.3795 0019774 237.9924 121.9337 14.30266755 02
| Epoch (UTC): | 25 May 2026 14:26:03 |
| Eccentricity: | 0.0019774 |
| inclination: | 98.7061° |
| perigee height: | 777 km |
| apogee height: | 805 km |
| right ascension of ascending node: | 147.3795° |
| argument of perigee: | 237.9924° |
| revolutions per day: | 14.30266755 |
| mean anomaly at epoch: | 121.9337° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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