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 33409U 26108.96242983 +.00000000 +00000-0 +50617-4 0 00005
2 33409 97.8618 127.8700 0017552 238.0180 121.9340 15.04119451 08
| Epoch (UTC): | 18 April 2026 23:05:53 |
| Eccentricity: | 0.0017552 |
| inclination: | 97.8618° |
| perigee height: | 542 km |
| apogee height: | 566 km |
| right ascension of ascending node: | 127.8700° |
| argument of perigee: | 238.0180° |
| revolutions per day: | 15.04119451 |
| mean anomaly at epoch: | 121.9340° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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