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 40336U 26053.86584859 +.00000000 +00000-0 -60525-5 0 00002
2 40336 98.3167 114.3605 0000554 51.7932 308.3304 14.35505505 07
| Epoch (UTC): | 22 February 2026 20:46:49 |
| Eccentricity: | 0.0000554 |
| inclination: | 98.3167° |
| perigee height: | 773 km |
| apogee height: | 774 km |
| right ascension of ascending node: | 114.3605° |
| argument of perigee: | 51.7932° |
| revolutions per day: | 14.35505505 |
| mean anomaly at epoch: | 308.3304° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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