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 26106.28156081 +.00000000 +00000-0 +29163-4 0 00000
2 40336 98.3413 165.0772 0000870 137.1293 222.9961 14.35542600 06
| Epoch (UTC): | 16 April 2026 06:45:26 |
| Eccentricity: | 0.0000870 |
| inclination: | 98.3413° |
| perigee height: | 773 km |
| apogee height: | 774 km |
| right ascension of ascending node: | 165.0772° |
| argument of perigee: | 137.1293° |
| revolutions per day: | 14.35542600 |
| mean anomaly at epoch: | 222.9961° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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