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 20442U 26145.29777486 +.00000000 +00000-0 +55405-4 0 00006
2 20442 98.8861 166.4716 0010425 273.7914 86.2077 14.34115051 05
| Epoch (UTC): | 25 May 2026 07:08:47 |
| Eccentricity: | 0.0010425 |
| inclination: | 98.8861° |
| perigee height: | 771 km |
| apogee height: | 785 km |
| right ascension of ascending node: | 166.4716° |
| argument of perigee: | 273.7914° |
| revolutions per day: | 14.34115051 |
| mean anomaly at epoch: | 86.2077° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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