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 26145.59313435 +.00000000 +00000-0 +79370-4 0 00000
2 40336 98.3543 203.1322 0002103 89.6836 270.4591 14.35502090 06
| Epoch (UTC): | 25 May 2026 14:14:06 |
| Eccentricity: | 0.0002103 |
| inclination: | 98.3543° |
| perigee height: | 772 km |
| apogee height: | 775 km |
| right ascension of ascending node: | 203.1322° |
| argument of perigee: | 89.6836° |
| revolutions per day: | 14.35502090 |
| mean anomaly at epoch: | 270.4591° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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