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 26075.03986872 +.00000000 +00000-0 +73193-4 0 00005
2 20442 98.8931 94.2467 0012561 117.2322 243.0143 14.34090825 00
| Epoch (UTC): | 16 March 2026 00:57:24 |
| Eccentricity: | 0.0012561 |
| inclination: | 98.8931° |
| perigee height: | 769 km |
| apogee height: | 787 km |
| right ascension of ascending node: | 94.2467° |
| argument of perigee: | 117.2322° |
| revolutions per day: | 14.34090825 |
| mean anomaly at epoch: | 243.0143° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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