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 20355U 26146.22946943 +.00000000 +00000-0 +00000-0 0 00006
2 20355 16.9034 340.9931 0291725 114.5393 254.7599 1.00734834 02
| Epoch (UTC): | 26 May 2026 05:30:26 |
| Eccentricity: | 0.0291725 |
| inclination: | 16.9034° |
| perigee height: | 34431 km |
| apogee height: | 36884 km |
| right ascension of ascending node: | 340.9931° |
| argument of perigee: | 114.5393° |
| revolutions per day: | 1.00734834 |
| mean anomaly at epoch: | 254.7599° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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